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41 Commits

Author SHA1 Message Date
Daniel Agar c11f61d57d commander: skip estimatorCheck for now 2024-02-15 15:46:31 -05:00
Daniel Agar d9a924225c simulator_mavlink: add heading_good_for_control 2024-02-15 15:46:14 -05:00
Daniel Agar 5f91c7fc2b simulation: HIL_STATE_QUATERNION add angular acceleration and protect from initial lat/lon 0 2024-02-15 15:20:33 -05:00
Daniel Agar 79538ac013 [WIP] simple simulation without sensor/estimator 2024-02-15 14:57:37 -05:00
Cyril C 74303a79e1 drivers/batt_smbus: fix BQ40Z80 timeout problem (#22751)
Co-authored-by: cyril.calvez <c.calvez@elistair.com>
2024-02-15 13:24:40 -05:00
Daniel Agar 8dc3975456 ekf2: only populate gnss pos aid src status if ref initialized
- this is a minor logging improvement when plotting the position from the beginning of the log (often a replay session)
2024-02-15 13:13:10 -05:00
Matthias Grob 84a7d42566 rover build: correct differential drive kconfig name 2024-02-15 10:08:51 -05:00
Matthias Grob f26df8492f Update GPS drivers to contain the astyle fix 2024-02-15 15:23:06 +01:00
Konrad cb09dde606 FixedwingPositionControl: Used corrected npfg roll output in path mode 2024-02-13 17:17:44 +01:00
Konrad 1a1891073e FixedwingPositionControl: Only warn user when roll is reduced for a longer period of time 2024-02-13 17:17:44 +01:00
Daniel Agar b8714f8980 ROMFS: rc.simulator EKF2 setup specific to gazebo classic 2024-02-13 11:14:44 -05:00
PX4 BuildBot 0c099f2b56 Update submodule gz to latest Tue Feb 13 12:39:17 UTC 2024
- gz in PX4/Firmware (c9ad60e3cc): https://github.com/PX4/PX4-gazebo-models/commit/c78f7f01417168e8faab7a83ade2129c0d26b39d
    - gz current upstream: https://github.com/PX4/PX4-gazebo-models/commit/f1c461fffb8567d6f0af770fb533f60f6ec62c22
    - Changes: https://github.com/PX4/PX4-gazebo-models/compare/c78f7f01417168e8faab7a83ade2129c0d26b39d...f1c461fffb8567d6f0af770fb533f60f6ec62c22

    f1c461f 2024-02-08 frederik - increase monocam clipping distance
6d5db73 2024-02-07 Sergei Grichine - Added Zero Turn Lawnmower model (#27)
5332071 2024-02-06 Frederik Markus - add navsat plugin to worlds and navsat sensor to models (#26)
2024-02-13 11:13:17 -05:00
Frederik Markus bb53781b8f simulation/gz_bridge: enable navsat plugin for accurate positioning of real life maps in Gazebo (#22638)
* publish the global groundtruth from the navsat callback and rearrange the local groundtruth as the altitude reference now has a dependency on the global groundtruth being initialized

---------

Signed-off-by: frederik <frederik.anilmarkus@gmail.com>
2024-02-13 11:09:35 -05:00
Silvan Fuhrer c9ad60e3cc Update src/modules/navigator/mission_block.cpp
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2024-02-13 10:34:57 +01:00
Silvan Fuhrer a6ef7b6da9 RTL: write out weather vane in comments (instead of WV)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
Silvan Fuhrer 6957818603 RTL: clean up naming of function arguments
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
Matthias Grob cb03835124 RTL: use dest.yaw instead of a separate heading_sp 2024-02-13 10:34:57 +01:00
Silvan Fuhrer b19e35ec7c RTL: change when to set a heading setpoint, generally leave it up to the executer
-remove RTL_HDG_MD
-only set heading setpoint in Navigator::RTL once above landing point,
or when RTL is triggered close to it
-never set a heading during RTL if weather vane is enabled

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
PX4 BuildBot dce53a626e boards: update all NuttX defconfigs 2024-02-12 08:58:49 -05:00
Daniel Agar 5f589bdda3 Update submodule GPSDrivers to latest Mon Feb 12 12:39:19 UTC 2024
- GPSDrivers in PX4/Firmware (17ff40898c683e1fe96ff9e2d2790594d188f872): https://github.com/PX4/PX4-GPSDrivers/commit/3393191fbb842f8e13a3f296218efec832640112
    - GPSDrivers current upstream: https://github.com/PX4/PX4-GPSDrivers/commit/f48cc01d31607baa4963bde090f530b44df3de12
    - Changes: https://github.com/PX4/PX4-GPSDrivers/compare/3393191fbb842f8e13a3f296218efec832640112...f48cc01d31607baa4963bde090f530b44df3de12

    f48cc01 2024-02-08 Julian Oes - ubx: separate config for jamming monitor
bc72f55 2024-02-08 Julian Oes - sbf: simplify odd define

Co-authored-by: PX4 BuildBot <bot@px4.io>
2024-02-12 08:58:21 -05:00
Matthias Grob 1998f54ea6 DifferentialDrive: move spoolup consideration to the main module 2024-02-12 14:29:10 +01:00
PerFrivik bef694f9ba Added spoolup and removed temporary timeout for EKF 2024-02-12 14:29:10 +01:00
PerFrivik 560d6a9d4b cleanup + updated acro 2024-02-12 14:29:10 +01:00
PerFrivik f996caa5bd Fixed bug in the guidance logic
After smoothing the linera velocity setpoint, the EKF has trouble initializing, becuase the acceleration is too smooth, to combat this issue, there is a 1 second delay when initializing the mission mode
2024-02-12 14:29:10 +01:00
PerFrivik bb0dfba4e6 added acro mode
Acro mode is manual mode, but with rate control
2024-02-12 14:29:10 +01:00
PerFrivik d197d94889 Fixed guidance logic and added feedforward term to compute the angular velocity 2024-02-12 14:29:10 +01:00
Matthias Grob 396ef222ee DifferentialDrive: Rework structure
3 Components Guidance - Control - Allocation
with their corresponding uORB interface.
2024-02-12 14:29:10 +01:00
Matthias Grob f85144ca76 DifferentialDrive: remove trailing zeros from prameter metadata 2024-02-12 14:29:10 +01:00
Matthias Grob b54b4f7dce Rename module differential_drive_control -> differential_drive 2024-02-12 14:29:10 +01:00
Matthias Grob fc90e235f1 Rename differential drive setpoint topics 2024-02-12 14:29:10 +01:00
Matthias Grob f7baeae1a0 DifferentialDriveControl: only save required parts of uORB message 2024-02-12 14:29:10 +01:00
PerFrivik e457a5baed Differential Drive Guidance: Add guidance
also add dependency on control allocation parameter CA_R_REV

Differential Drive Guidance: Added mission logic

Differential Drive Guidance

Differential Drive Guidance

Differential Guidance: Inlcude library

Differential Guidance: Compiles, does not work though

Differential Guidance: Works somewhat

Differential Guidance: Temp

Differential Guidance: Tuning

Differeital Drive Guidance: Remove waypoint mover

Differential Guidance: Fixed accuracy issue by converting from float to double

Differential Guidance: rebased on differentialdrive and improved waypoint accuracy

Temp

Differential Guidance: cleanup

temp
2024-02-12 14:29:10 +01:00
PX4 BuildBot 0f3925b21d update all px4board kconfig 2024-02-09 10:48:26 -05:00
muramura f636414ca7 tuning_tools: Change 1G to a more accurate value 2024-02-09 10:26:57 -05:00
muramura 00a9e4c76b Auto: Change 1G to a more accurate value 2024-02-09 10:26:57 -05:00
Alex Klimaj 31bbda0b58 boards: new ARK Septentrio GPS CAN node(ark_septentrio-gps)
* update gps submodule with sbf fix
* ARK Septentrio GPS initial commit
2024-02-09 10:26:09 -05:00
Matthias Grob b355c16141 Lanbao driver: correct rangefinder type to IR 2024-02-09 06:19:12 +01:00
Matthias Grob 7fdb5ef3cb PWMOut/px4io: correct automatic servo/motor configuration messages 2024-02-09 06:19:12 +01:00
fury1895 3de7d83e5f v6x board_sensors: publish system_power if ADC_ADS1115_EN is enabled 2024-02-08 16:11:34 +01:00
Matthias Grob 97cb933cff FLightTaskAuto: limit nudging speed based on distance sensor 2024-02-07 11:23:55 +01:00
Silvan Fuhrer 584d8abe1e params: change return type of param_modify_on_import to enum
Return early in param_import_callback() with 1 if we do a param_set in the param translation.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-07 08:08:37 +01:00
88 changed files with 3114 additions and 438 deletions
+1
View File
@@ -25,6 +25,7 @@ jobs:
ark_can-rtk-gps,
ark_cannode,
ark_fmu-v6x,
ark_septentrio-gps,
atl_mantis-edu,
av_x-v1,
bitcraze_crazyflie,
+10
View File
@@ -151,6 +151,16 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: ark_can-rtk-gps_canbootloader
ark_septentrio_gps_default:
short: ark_septentrio_gps_default
buildType: MinSizeRel
settings:
CONFIG: ark_septentrio_gps_default
ark_septentrio_gps_canbootloader:
short: ark_septentrio_gps_canbootloader
buildType: MinSizeRel
settings:
CONFIG: ark_septentrio_gps_canbootloader
ark_cannode_default:
short: ark_cannode_default
buildType: MinSizeRel
@@ -41,19 +41,6 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" = "1" ]; then
echo "INFO [init] Gazebo simulator"
# set local coordinate frame reference
if [ -n "${PX4_HOME_LAT}" ]; then
param set SIM_GZ_HOME_LAT ${PX4_HOME_LAT}
fi
if [ -n "${PX4_HOME_LON}" ]; then
param set SIM_GZ_HOME_LON ${PX4_HOME_LON}
fi
if [ -n "${PX4_HOME_ALT}" ]; then
param set SIM_GZ_HOME_ALT ${PX4_HOME_ALT}
fi
# Only start up Gazebo if PX4_GZ_STANDALONE is not set.
if [ -z "${PX4_GZ_STANDALONE}" ]; then
@@ -180,6 +167,12 @@ elif [ "$PX4_SIM_MODEL" = "jmavsim_iris" ] || [ "$(param show -q SYS_AUTOSTART)"
else
# otherwise start simulator (mavlink) module
# EKF2 specifics
param set-default EKF2_GPS_DELAY 10
param set-default EKF2_MULTI_IMU 3
param set-default SENS_IMU_MODE 0
simulator_tcp_port=$((4560+px4_instance))
# Check if PX4_SIM_HOSTNAME environment variable is empty
+1 -5
View File
@@ -164,10 +164,6 @@ param set-default COM_RC_IN_MODE 1
# Speedup SITL startup
param set-default EKF2_REQ_GPS_H 0.5
# Multi-EKF
param set-default EKF2_MULTI_IMU 3
param set-default SENS_IMU_MODE 0
param set-default IMU_GYRO_FFT_EN 1
param set-default MAV_PROTO_VER 2 # Ensures QGC does not drop the first few packets after a SITL restart due to MAVLINK 1 packets
@@ -257,7 +253,7 @@ fi
tone_alarm start
rc_update start
manual_control start
sensors start
#sensors start
commander start
if ! pwm_out_sim start -m sim
@@ -5,7 +5,7 @@
ekf2 start &
# Start rover differential drive controller.
differential_drive_control start
differential_drive start
# Start Land Detector.
land_detector start rover
@@ -0,0 +1,5 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT=""
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BOOTLOADERS=y
@@ -0,0 +1,37 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
CONFIG_DRIVERS_MAGNETOMETER_BOSCH_BMM150=y
CONFIG_DRIVERS_SAFETY_BUTTON=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_UAVCANNODE_BEEP_COMMAND=y
CONFIG_UAVCANNODE_GNSS_FIX=y
CONFIG_UAVCANNODE_LIGHTS_COMMAND=y
CONFIG_UAVCANNODE_MAGNETIC_FIELD_STRENGTH=y
CONFIG_UAVCANNODE_RTK_DATA=y
CONFIG_UAVCANNODE_SAFETY_BUTTON=y
CONFIG_UAVCANNODE_STATIC_PRESSURE=y
CONFIG_UAVCANNODE_STATIC_TEMPERATURE=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
CONFIG_MODULES_SENSORS=y
# CONFIG_SENSORS_VEHICLE_AIRSPEED is not set
# CONFIG_SENSORS_VEHICLE_AIR_DATA is not set
# CONFIG_SENSORS_VEHICLE_GPS_POSITION is not set
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_PERF=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_VER=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
@@ -0,0 +1,13 @@
{
"board_id": 84,
"magic": "PX4FWv1",
"description": "Firmware for the ARK Septentrio GPS board",
"image": "",
"build_time": 0,
"summary": "ARKSEPTENTRIOGPS",
"version": "0.1",
"image_size": 0,
"image_maxsize": 2080768,
"git_identity": "",
"board_revision": 0
}
@@ -0,0 +1,13 @@
#!/bin/sh
#
# board specific defaults
#------------------------------------------------------------------------------
param set-default CBRK_IO_SAFETY 0
param set-default CANNODE_SUB_MBD 1
param set-default CANNODE_SUB_RTCM 1
param set-default MBE_ENABLE 1
param set-default SENS_IMU_CLPNOTI 0
safety_button start
tone_alarm start
@@ -0,0 +1,11 @@
#!/bin/sh
#
# board sensors init
#------------------------------------------------------------------------------
gps start -d /dev/ttyS0 -p sbf
icm42688p -R 0 -s start
bmp388 -I -b 1 start
bmm150 -I -b 1 start
@@ -0,0 +1,56 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/septentrio-gps/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=4096
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BINFMT_DISABLE=y
CONFIG_BOARDCTL=y
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEBUG_TCBINFO=y
CONFIG_DEFAULT_SMALL=y
CONFIG_DISABLE_MOUNTPOINT=y
CONFIG_EXPERIMENTAL=y
CONFIG_FDCLONE_DISABLE=y
CONFIG_FDCLONE_STDIO=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_IDLETHREAD_STACKSIZE=4096
CONFIG_INIT_STACKSIZE=4096
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_STRERROR=y
CONFIG_MM_REGIONS=2
CONFIG_NAME_MAX=0
CONFIG_NUNGET_CHARS=0
CONFIG_PREALLOC_TIMERS=0
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20010000
CONFIG_RAW_BINARY=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_DISABLE_BUFFERING=y
CONFIG_STM32_NOEXT_VECTORS=y
CONFIG_STM32_TIM8=y
CONFIG_TASK_NAME_SIZE=0
CONFIG_USEC_PER_TICK=1000
@@ -0,0 +1,152 @@
/************************************************************************************
* configs/px4fmu/include/board.h
* include/arch/board/board.h
*
* Copyright (C) 2009 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
************************************************************************************/
#include "board_dma_map.h"
#ifndef __ARCH_BOARD_BOARD_H
#define __ARCH_BOARD_BOARD_H
#include <nuttx/config.h>
#ifndef __ASSEMBLY__
# include <stdint.h>
#endif
#include <stm32.h>
/* HSI - 8 MHz RC factory-trimmed
* LSI - 32 KHz RC
* HSE - 8 MHz Crystal
* LSE - not installed
*/
#define STM32_BOARD_USEHSE 1
#define STM32_BOARD_XTAL 8000000
#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL
#define STM32_HSI_FREQUENCY 16000000ul
#define STM32_LSI_FREQUENCY 32000
/* Main PLL Configuration */
#define STM32_PLLCFG_PLLM RCC_PLLCFG_PLLM(8)
#define STM32_PLLCFG_PLLN RCC_PLLCFG_PLLN(384)
#define STM32_PLLCFG_PLLP RCC_PLLCFG_PLLP_4
#define STM32_PLLCFG_PLLQ RCC_PLLCFG_PLLQ(8)
#define STM32_PLLCFG_PLLR RCC_PLLCFG_PLLR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SM RCC_PLLI2SCFGR_PLLI2SM(16)
#define STM32_RCC_PLLI2SCFGR_PLLI2SN RCC_PLLI2SCFGR_PLLI2SN(192)
#define STM32_RCC_PLLI2SCFGR_PLLI2SQ RCC_PLLI2SCFGR_PLLI2SQ(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SR RCC_PLLI2SCFGR_PLLI2SR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SSRC RCC_PLLI2SCFGR_PLLI2SSRC(0) /* HSE or HSI depending on PLLSRC of PLLCFGR*/
#define STM32_RCC_DCKCFGR2_CK48MSEL RCC_DCKCFGR2_CK48MSEL_PLL
#define STM32_RCC_DCKCFGR2_FMPI2C1SEL RCC_DCKCFGR2_FMPI2C1SEL_APB
#define STM32_RCC_DCKCFGR2_SDIOSEL RCC_DCKCFGR2_SDIOSEL_48MHZ
#define STM32_SYSCLK_FREQUENCY 96000000ul
/* AHB clock (HCLK) is SYSCLK (96MHz) */
#define STM32_RCC_CFGR_HPRE RCC_CFGR_HPRE_SYSCLK /* HCLK = SYSCLK / 1 */
#define STM32_HCLK_FREQUENCY STM32_SYSCLK_FREQUENCY
#define STM32_BOARD_HCLK STM32_HCLK_FREQUENCY /* Same as above, to satisfy compiler */
/* APB1 clock (PCLK1) is HCLK/2 (48MHz) */
#define STM32_RCC_CFGR_PPRE1 RCC_CFGR_PPRE1_HCLKd2 /* PCLK1 = HCLK / 2 */
#define STM32_PCLK1_FREQUENCY (STM32_HCLK_FREQUENCY/2)
/* Timers driven from APB1 will be twice PCLK1 (see page 112 of reference manual) */
#define STM32_APB1_TIM2_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM3_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM4_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM5_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM12_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM13_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM14_CLKIN (2*STM32_PCLK1_FREQUENCY)
/* APB2 clock (PCLK2) is HCLK (96MHz) */
#define STM32_RCC_CFGR_PPRE2 RCC_CFGR_PPRE2_HCLK /* PCLK2 = HCLK */
#define STM32_PCLK2_FREQUENCY (STM32_HCLK_FREQUENCY)
/* Timers driven from APB2 will be PCLK2 since no prescale division */
#define STM32_APB2_TIM1_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM8_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM9_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM10_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM11_CLKIN (STM32_PCLK2_FREQUENCY)
/* Timer Frequencies, if APBx is set to 1, frequency is same to APBx otherwise frequency is 2xAPBx. */
#define BOARD_TIM2_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM3_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM4_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM5_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM6_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM7_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM8_FREQUENCY (2 * STM32_PCLK2_FREQUENCY)
/* Alternate function pin selections ************************************************/
/* UARTs */
#define GPIO_USART1_RX GPIO_USART1_RX_2
#define GPIO_USART1_TX GPIO_USART1_TX_3
#define GPIO_USART2_RX GPIO_USART2_RX_1
#define GPIO_USART2_TX GPIO_USART2_TX_1
/* CAN */
#define GPIO_CAN1_RX GPIO_CAN1_RX_1
#define GPIO_CAN1_TX GPIO_CAN1_TX_1
/* I2C */
#define GPIO_MCU_I2C1_SCL
#define GPIO_MCU_I2C1_SDA
#define GPIO_I2C1_SCL GPIO_I2C1_SCL_1
#define GPIO_I2C1_SDA GPIO_I2C1_SDA_1
#define GPIO_I2C1_SCL_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN6)
#define GPIO_I2C1_SDA_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN7)
#define GPIO_I2C2_SCL GPIO_I2C2_SCL_1
#define GPIO_I2C2_SDA GPIO_I2C2_SDA_4
#define GPIO_I2C2_SCL_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN9)
#define GPIO_I2C2_SDA_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN10)
/* SPI */
#define GPIO_SPI1_MISO GPIO_SPI1_MISO_1
#define GPIO_SPI1_MOSI GPIO_SPI1_MOSI_1
#define GPIO_SPI1_SCK GPIO_SPI1_SCK_1
#endif /* __ARCH_BOARD_BOARD_H */
@@ -0,0 +1,46 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#pragma once
// DMA1 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
// DMA2 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
#define DMACHAN_SPI1_RX DMAMAP_SPI1_RX_1 // DMA2, Stream 0, Channel 3
#define DMACHAN_SPI1_TX DMAMAP_SPI1_TX_1 // DMA2, Stream 3, Channel 3
#define DMACHAN_USART1_RX DMAMAP_USART1_RX_1 // DMA2, Stream 2, Channel 4
#define DMAMAP_USART1_RX DMAMAP_USART1_RX_1
//#define DMACHAN_USART1_TX DMAMAP_USART1_TX // DMA2, Stream 7, Channel 4
@@ -0,0 +1,152 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
# CONFIG_DISABLE_ENVIRON is not set
# CONFIG_DISABLE_PSEUDOFS_OPERATIONS is not set
# CONFIG_DISABLE_PTHREAD is not set
# CONFIG_NSH_DISABLEBG is not set
# CONFIG_NSH_DISABLESCRIPT is not set
# CONFIG_NSH_DISABLE_CAT is not set
# CONFIG_NSH_DISABLE_CD is not set
# CONFIG_NSH_DISABLE_CP is not set
# CONFIG_NSH_DISABLE_DATE is not set
# CONFIG_NSH_DISABLE_DF is not set
# CONFIG_NSH_DISABLE_ECHO is not set
# CONFIG_NSH_DISABLE_ENV is not set
# CONFIG_NSH_DISABLE_EXEC is not set
# CONFIG_NSH_DISABLE_EXPORT is not set
# CONFIG_NSH_DISABLE_FREE is not set
# CONFIG_NSH_DISABLE_GET is not set
# CONFIG_NSH_DISABLE_HELP is not set
# CONFIG_NSH_DISABLE_ITEF is not set
# CONFIG_NSH_DISABLE_KILL is not set
# CONFIG_NSH_DISABLE_LOOPS is not set
# CONFIG_NSH_DISABLE_LS is not set
# CONFIG_NSH_DISABLE_MKDIR is not set
# CONFIG_NSH_DISABLE_MOUNT is not set
# CONFIG_NSH_DISABLE_MV is not set
# CONFIG_NSH_DISABLE_PS is not set
# CONFIG_NSH_DISABLE_PSSTACKUSAGE is not set
# CONFIG_NSH_DISABLE_PWD is not set
# CONFIG_NSH_DISABLE_RM is not set
# CONFIG_NSH_DISABLE_RMDIR is not set
# CONFIG_NSH_DISABLE_SEMICOLON is not set
# CONFIG_NSH_DISABLE_SET is not set
# CONFIG_NSH_DISABLE_SLEEP is not set
# CONFIG_NSH_DISABLE_SOURCE is not set
# CONFIG_NSH_DISABLE_TEST is not set
# CONFIG_NSH_DISABLE_TIME is not set
# CONFIG_NSH_DISABLE_UMOUNT is not set
# CONFIG_NSH_DISABLE_UNSET is not set
# CONFIG_NSH_DISABLE_USLEEP is not set
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/septentrio-gps/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=768
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
CONFIG_BOARD_ASSERT_RESET_VALUE=0
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_HARDFAULT_ALERT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEBUG_TCBINFO=y
CONFIG_DEFAULT_SMALL=y
CONFIG_FDCLONE_STDIO=y
CONFIG_FS_CROMFS=y
CONFIG_FS_ROMFS=y
CONFIG_GRAN=y
CONFIG_GRAN_INTR=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_I2C=y
CONFIG_I2C_RESET=y
CONFIG_IDLETHREAD_STACKSIZE=750
CONFIG_INIT_ENTRYPOINT="nsh_main"
CONFIG_INIT_STACKSIZE=2624
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_MAX_EXITFUNS=1
CONFIG_MEMSET_64BIT=y
CONFIG_MEMSET_OPTSPEED=y
CONFIG_MM_REGIONS=2
CONFIG_NAME_MAX=40
CONFIG_NSH_ARCHINIT=y
CONFIG_NSH_ARGCAT=y
CONFIG_NSH_BUILTIN_APPS=y
CONFIG_NSH_CMDPARMS=y
CONFIG_NSH_CROMFSETC=y
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
CONFIG_NSH_QUOTE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_VARS=y
CONFIG_PREALLOC_TIMERS=50
CONFIG_PTHREAD_MUTEX_ROBUST=y
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20000000
CONFIG_RAW_BINARY=y
CONFIG_SCHED_HPWORK=y
CONFIG_SCHED_HPWORKPRIORITY=249
CONFIG_SCHED_HPWORKSTACKSIZE=1280
CONFIG_SCHED_INSTRUMENTATION=y
CONFIG_SCHED_INSTRUMENTATION_EXTERNAL=y
CONFIG_SCHED_INSTRUMENTATION_SWITCH=y
CONFIG_SCHED_WAITPID=y
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_SIG_SIGWORK=4
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_BUFFER_SIZE=32
CONFIG_STM32_ADC1=y
CONFIG_STM32_DISABLE_IDLE_SLEEP_DURING_DEBUG=y
CONFIG_STM32_DMA1=y
CONFIG_STM32_DMA2=y
CONFIG_STM32_FLASH_PREFETCH=y
CONFIG_STM32_FLOWCONTROL_BROKEN=y
CONFIG_STM32_I2C1=y
CONFIG_STM32_I2C2=y
CONFIG_STM32_JTAG_SW_ENABLE=y
CONFIG_STM32_PWR=y
CONFIG_STM32_SERIALBRK_BSDCOMPAT=y
CONFIG_STM32_SERIAL_DISABLE_REORDERING=y
CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI1_DMA=y
CONFIG_STM32_SPI1_DMA_BUFFER=1024
CONFIG_STM32_TIM8=y
CONFIG_STM32_USART1=y
CONFIG_STM32_USART2=y
CONFIG_STM32_USART_BREAKS=y
CONFIG_STM32_WWDG=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_USART1_BAUD=57600
CONFIG_USART1_RXBUFSIZE=2000
CONFIG_USART1_RXDMA=y
CONFIG_USART1_TXBUFSIZE=2000
CONFIG_USART2_BAUD=57600
CONFIG_USART2_RXBUFSIZE=600
CONFIG_USART2_SERIAL_CONSOLE=y
CONFIG_USART2_TXBUFSIZE=1100
CONFIG_USEC_PER_TICK=1000
@@ -0,0 +1,134 @@
/****************************************************************************
* nuttx-config/scripts/canbootloader_script.ld
*
* Copyright (C) 2015 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/* The STM32F412 has 512Kb of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08000000, LENGTH = 32K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
@@ -0,0 +1,146 @@
/****************************************************************************
* scripts/ld.script
*
* Copyright (C) 2011 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name NuttX nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/* The STM32F412 has 512Kb of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08010000, LENGTH = 928K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
EXTERN(_bootdelay_signature)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
. = ALIGN(8);
/*
* This section positions the app_descriptor_t used
* by the make_can_boot_descriptor.py tool to set
* the application image's descriptor so that the
* uavcan bootloader has the ability to validate the
* image crc, size etc
*/
KEEP(*(.app_descriptor))
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
@@ -0,0 +1,67 @@
############################################################################
#
# Copyright (c) 2020 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
if("${PX4_BOARD_LABEL}" STREQUAL "canbootloader")
add_library(drivers_board
boot_config.h
boot.c
led.c
led.h
)
target_link_libraries(drivers_board
PRIVATE
nuttx_arch
nuttx_drivers
canbootloader
)
target_include_directories(drivers_board PRIVATE ${PX4_SOURCE_DIR}/platforms/nuttx/src/canbootloader)
else()
add_library(drivers_board
can.c
i2c.cpp
init.c
led.c
spi.cpp
)
target_link_libraries(drivers_board
PRIVATE
arch_spi
drivers__led # drv_led_start
nuttx_arch
nuttx_drivers
px4_layer
)
endif()
@@ -0,0 +1,125 @@
/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file board_config.h
*
* board internal definitions
*/
#pragma once
#include <px4_platform_common/px4_config.h>
#include <nuttx/compiler.h>
#include <stdint.h>
/* BUTTON */
#define GPIO_BTN_SAFETY /* PB15 */ (GPIO_INPUT|GPIO_PULLDOWN|GPIO_PORTB|GPIO_PIN15)
/* Safety LED */
#define GPIO_LED_SAFETY /* PA1 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_SET|GPIO_PORTA|GPIO_PIN1)
/* Tone alarm output. */
#define TONE_ALARM_TIMER 2 /* timer 2 */
#define TONE_ALARM_CHANNEL 1 /* channel 1 */
#define GPIO_TONE_ALARM_IDLE /* PA0 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN0)
#define GPIO_TONE_ALARM /* PA0 */ (GPIO_ALT|GPIO_AF1|GPIO_SPEED_2MHz|GPIO_PUSHPULL|GPIO_PORTA|GPIO_PIN0)
/* CAN Silent mode control */
#define GPIO_CAN1_SILENT_S0 /* PB12 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN12)
/* CAN termination software control */
#define GPIO_CAN1_TERMINATION /* PB13 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN13)
#define GPIO_CAN_TERM GPIO_CAN1_TERMINATION
/* ICM42688p FSYNC */
#define GPIO_42688P_FSYNC /* PB8 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN8)
/* Boot config */
#define GPIO_BOOT_CONFIG /* PC15 */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTC|GPIO_PIN15|GPIO_EXTI)
/* LEDs are driven with open drain to support Anode to 5V or 3.3V */
#define GPIO_TIM1_CH1 /* PA8 */ (GPIO_TIM1_CH1_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define GPIO_TIM1_CH2 /* PA9 */ (GPIO_TIM1_CH2_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define GPIO_TIM1_CH3 /* PA10 */ (GPIO_TIM1_CH3_1|GPIO_OPENDRAIN|GPIO_SPEED_2MHz)
#define GPIO_I2C1_SCL_RESET /* PB6 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN6)
#define GPIO_I2C1_SDA_RESET /* PB7 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN7)
#define GPIO_I2C2_SCL_RESET /* PB10 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN10)
#define GPIO_I2C2_SDA_RESET /* PB9 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN9)
#define GPIO_I2C2_SCL_RESET /* PB10 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN10)
#define GPIO_I2C2_SDA_RESET /* PB9 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTB|GPIO_PIN9)
#define GPIO_USART1_RX_GPIO (GPIO_INPUT|GPIO_PULLUP|GPIO_SPEED_50MHz|GPIO_PORTB|GPIO_PIN3)
#define GPIO_USART1_TX_GPIO (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_PULLUP|GPIO_SPEED_50MHz|GPIO_PORTA|GPIO_PIN15)
#define GPIO_USART2_RX_GPIO (GPIO_INPUT|GPIO_PULLUP|GPIO_SPEED_50MHz|GPIO_PORTA|GPIO_PIN3)
#define GPIO_USART2_TX_GPIO (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_PULLUP|GPIO_SPEED_50MHz|GPIO_PORTA|GPIO_PIN2)
#define FLASH_BASED_PARAMS
/* High-resolution timer */
#define HRT_TIMER 3 /* use timer 3 for the HRT */
#define HRT_TIMER_CHANNEL 4 /* use capture/compare channel 4 */
#define PX4_GPIO_INIT_LIST { \
GPIO_BTN_SAFETY, \
GPIO_LED_SAFETY, \
GPIO_I2C1_SCL_RESET, \
GPIO_I2C1_SDA_RESET, \
GPIO_I2C2_SCL_RESET, \
GPIO_I2C2_SDA_RESET, \
GPIO_42688P_FSYNC, \
GPIO_BOOT_CONFIG, \
GPIO_CAN1_TX, \
GPIO_CAN1_RX, \
GPIO_CAN1_SILENT_S0, \
GPIO_CAN1_TERMINATION, \
}
__BEGIN_DECLS
#define BOARD_HAS_N_S_RGB_LED 1
#define BOARD_MAX_LEDS BOARD_HAS_N_S_RGB_LED
#ifndef __ASSEMBLY__
extern void stm32_spiinitialize(void);
#include <px4_platform_common/board_common.h>
#endif /* __ASSEMBLY__ */
__END_DECLS
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
* Author: Ben Dyer <ben_dyer@mac.com>
* Pavel Kirienko <pavel.kirienko@zubax.com>
* David Sidrane <david_s5@nscdg.com>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/****************************************************************************
* Included Files
****************************************************************************/
#include <px4_config.h>
#include <stdint.h>
#include "boot_config.h"
#include "board.h"
#include <debug.h>
#include <string.h>
#include <arch/board/board.h>
#include <nuttx/board.h>
#include "led.h"
/************************************************************************************
* Name: stm32_boardinitialize
*
* Description:
* All STM32 architectures must provide the following entry point. This entry point
* is called early in the initialization -- after all memory has been configured
* and mapped but before any devices have been initialized.
*
************************************************************************************/
__EXPORT void stm32_boardinitialize(void)
{
putreg32(getreg32(STM32_RCC_APB1ENR) | RCC_APB1ENR_CAN1EN, STM32_RCC_APB1ENR);
stm32_configgpio(GPIO_CAN1_RX);
stm32_configgpio(GPIO_CAN1_TX);
stm32_configgpio(GPIO_CAN1_SILENT_S0);
stm32_configgpio(GPIO_CAN1_TERMINATION);
putreg32(getreg32(STM32_RCC_APB1RSTR) | RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
putreg32(getreg32(STM32_RCC_APB1RSTR) & ~RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
#if defined(OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO)
stm32_configgpio(GPIO_GETNODEINFO_JUMPER);
#endif
}
/************************************************************************************
* Name: board_deinitialize
*
* Description:
* This function is called by the bootloader code prior to booting
* the application. Is should place the HW into an benign initialized state.
*
************************************************************************************/
void board_deinitialize(void)
{
putreg32(getreg32(STM32_RCC_APB1RSTR) | RCC_APB1RSTR_CAN1RST, STM32_RCC_APB1RSTR);
}
/****************************************************************************
* Name: board_get_product_name
*
* Description:
* Called to retrieve the product name. The returned value is a assumed
* to be written to a pascal style string that will be length prefixed
* and not null terminated
*
* Input Parameters:
* product_name - A pointer to a buffer to write the name.
* maxlen - The maximum number of charter that can be written
*
* Returned Value:
* The length of characters written to the buffer.
*
****************************************************************************/
uint8_t board_get_product_name(uint8_t *product_name, size_t maxlen)
{
DEBUGASSERT(maxlen > UAVCAN_STRLEN(HW_UAVCAN_NAME));
memcpy(product_name, HW_UAVCAN_NAME, UAVCAN_STRLEN(HW_UAVCAN_NAME));
return UAVCAN_STRLEN(HW_UAVCAN_NAME);
}
/****************************************************************************
* Name: board_get_hardware_version
*
* Description:
* Called to retrieve the hardware version information. The function
* will first initialize the the callers struct to all zeros.
*
* Input Parameters:
* hw_version - A pointer to a uavcan_hardwareversion_t.
*
* Returned Value:
* Length of the unique_id
*
****************************************************************************/
size_t board_get_hardware_version(uavcan_HardwareVersion_t *hw_version)
{
memset(hw_version, 0, sizeof(uavcan_HardwareVersion_t));
hw_version->major = HW_VERSION_MAJOR;
hw_version->minor = HW_VERSION_MINOR;
return board_get_mfguid(*(mfguid_t *) hw_version->unique_id);
}
/****************************************************************************
* Name: board_indicate
*
* Description:
* Provides User feedback to indicate the state of the bootloader
* on board specific hardware.
*
* Input Parameters:
* indication - A member of the uiindication_t
*
* Returned Value:
* None
*
****************************************************************************/
#define led(n, code, r , g , b, h) {.red = (r),.green = (g), .blue = (b),.hz = (h)}
typedef begin_packed_struct struct led_t {
uint8_t red;
uint8_t green;
uint8_t blue;
uint8_t hz;
} end_packed_struct led_t;
static const led_t i2l[] = {
led(0, off, 0, 0, 0, 0),
led(1, reset, 128, 128, 128, 30),
led(2, autobaud_start, 0, 128, 0, 1),
led(3, autobaud_end, 0, 128, 0, 2),
led(4, allocation_start, 0, 0, 64, 2),
led(5, allocation_end, 0, 128, 64, 3),
led(6, fw_update_start, 32, 128, 64, 3),
led(7, fw_update_erase_fail, 32, 128, 32, 3),
led(8, fw_update_invalid_response, 64, 0, 0, 1),
led(9, fw_update_timeout, 64, 0, 0, 2),
led(a, fw_update_invalid_crc, 64, 0, 0, 4),
led(b, jump_to_app, 0, 128, 0, 10),
};
void board_indicate(uiindication_t indication)
{
rgb_led(i2l[indication].red,
i2l[indication].green,
i2l[indication].blue,
i2l[indication].hz);
}
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/*
* @file boot_config.h
*
* bootloader definitions that configures the behavior and options
* of the Boot loader
* This file is relies on the parent folder's boot_config.h file and defines
* different usages of the hardware for bootloading
*/
#pragma once
/************************************************************************************
* Included Files
************************************************************************************/
/* Bring in the board_config.h definitions
* todo:make this be pulled in from a targed's build
* files in nuttx*/
#include "board_config.h"
#include "uavcan.h"
#include <nuttx/compiler.h>
#include <stdint.h>
#include <stm32_flash.h>
/****************************************************************************
* Pre-processor Definitions
****************************************************************************/
#define OPT_PREFERRED_NODE_ID ANY_NODE_ID
//todo:wrap OPT_x in in ifdefs for command line definitions
#define OPT_TBOOT_MS 3000
#define OPT_NODE_STATUS_RATE_MS 800
#define OPT_NODE_INFO_RATE_MS 50
#define OPT_BL_NUMBER_TIMERS 7
/*
* This Option set is set to 1 ensure a provider of firmware has an
* opportunity update the node's firmware.
* This Option is the default policy and can be overridden by
* a jumper
* When this Policy is set, the node will ignore tboot and
* wait indefinitely for a GetNodeInfo request before booting.
*
* OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO_INVERT is used to allow
* the polarity of the jumper to be True Active
*
* wait OPT_WAIT_FOR_GETNODEINFO OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO
* Jumper
* yes 1 0 x
* yes 1 1 Active
* no 1 1 Not Active
* no 0 0 X
* yes 0 1 Active
* no 0 1 Not Active
*
*/
#define OPT_WAIT_FOR_GETNODEINFO 0
#define OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO 1
#define OPT_WAIT_FOR_GETNODEINFO_JUMPER_GPIO_INVERT 1
#define OPT_ENABLE_WD 1
#define OPT_RESTART_TIMEOUT_MS 20000
/* Reserved for the Booloader */
#define OPT_BOOTLOADER_SIZE_IN_K (1024*64)
/* Reserved for the application out of the total
* system flash minus the BOOTLOADER_SIZE_IN_K
*/
#define OPT_APPLICATION_RESERVER_IN_K 0
#define OPT_APPLICATION_IMAGE_OFFSET OPT_BOOTLOADER_SIZE_IN_K
#define OPT_APPLICATION_IMAGE_LENGTH (FLASH_SIZE-(OPT_BOOTLOADER_SIZE_IN_K+OPT_APPLICATION_RESERVER_IN_K))
#define FLASH_BASE STM32_FLASH_BASE
#define FLASH_SIZE STM32_FLASH_SIZE
#define APPLICATION_LOAD_ADDRESS (FLASH_BASE + OPT_APPLICATION_IMAGE_OFFSET)
#define APPLICATION_SIZE (FLASH_SIZE-OPT_APPLICATION_IMAGE_OFFSET)
#define APPLICATION_LAST_8BIT_ADDRRESS ((uint8_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint8_t)))
#define APPLICATION_LAST_32BIT_ADDRRESS ((uint32_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint32_t)))
#define APPLICATION_LAST_64BIT_ADDRRESS ((uint64_t *)((APPLICATION_LOAD_ADDRESS+APPLICATION_SIZE)-sizeof(uint64_t)))
/* If this board uses big flash that have large sectors */
#define OPT_USE_YIELD
/* Bootloader Option*****************************************************************
*
*/
#define GPIO_GETNODEINFO_JUMPER (GPIO_BOOT_CONFIG & ~GPIO_EXTI)
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/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file can.c
*
* Board-specific CAN functions.
*/
/************************************************************************************
* Included Files
************************************************************************************/
#include <px4_platform_common/px4_config.h>
#include <errno.h>
#include <debug.h>
#include <nuttx/can/can.h>
#include <arch/board/board.h>
#include "chip.h"
#include "arm_internal.h"
#include "stm32.h"
#include "stm32_can.h"
#include "board_config.h"
#ifdef CONFIG_CAN
/************************************************************************************
* Pre-processor Definitions
************************************************************************************/
/* Configuration ********************************************************************/
#if defined(CONFIG_STM32_CAN1) && defined(CONFIG_STM32_CAN2)
# warning "Both CAN1 and CAN2 are enabled. Assuming only CAN1."
# undef CONFIG_STM32_CAN2
#endif
#ifdef CONFIG_STM32_CAN1
# define CAN_PORT 1
#else
# define CAN_PORT 2
#endif
/************************************************************************************
* Private Functions
************************************************************************************/
/************************************************************************************
* Public Functions
************************************************************************************/
int can_devinit(void);
/************************************************************************************
* Name: can_devinit
*
* Description:
* All STM32 architectures must provide the following interface to work with
* examples/can.
*
************************************************************************************/
int can_devinit(void)
{
static bool initialized = false;
struct can_dev_s *can;
int ret;
/* Check if we have already initialized */
if (!initialized) {
/* Call stm32_caninitialize() to get an instance of the CAN interface */
can = stm32_caninitialize(CAN_PORT);
if (can == NULL) {
canerr("ERROR: Failed to get CAN interface\n");
return -ENODEV;
}
/* Register the CAN driver at "/dev/can0" */
ret = can_register("/dev/can0", can);
if (ret < 0) {
canerr("ERROR: can_register failed: %d\n", ret);
return ret;
}
/* Now we are initialized */
initialized = true;
}
return OK;
}
#endif
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/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include <px4_arch/i2c_hw_description.h>
constexpr px4_i2c_bus_t px4_i2c_buses[I2C_BUS_MAX_BUS_ITEMS] = {
initI2CBusInternal(1),
initI2CBusInternal(2),
};
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file init.c
*
* board specific early startup code. This file implements the
* board_app_initialize() function that is called early by nsh during startup.
*
* Code here is run before the rcS script is invoked; it should start required
* subsystems and perform board-specific initialization.
*/
#include <px4_platform_common/px4_config.h>
#include <px4_platform_common/tasks.h>
#include <stdbool.h>
#include <stdio.h>
#include <string.h>
#include <debug.h>
#include <errno.h>
#include <syslog.h>
#include <nuttx/board.h>
#include <stm32.h>
#include "board_config.h"
#include "led.h"
#include <stm32_uart.h>
#include <arch/board/board.h>
#include <drivers/drv_hrt.h>
#include <drivers/drv_board_led.h>
#include <drivers/drv_watchdog.h>
#include <systemlib/px4_macros.h>
#include <px4_platform_common/init.h>
#include <px4_platform/gpio.h>
# if defined(FLASH_BASED_PARAMS)
# include <parameters/flashparams/flashfs.h>
#endif
/************************************************************************************
* Name: stm32_boardinitialize
*
* Description:
* All STM32 architectures must provide the following entry point. This entry point
* is called early in the initialization -- after all memory has been configured
* and mapped but before any devices have been initialized.
*
************************************************************************************/
__EXPORT void stm32_boardinitialize(void)
{
watchdog_init();
/* configure pins */
const uint32_t gpio[] = PX4_GPIO_INIT_LIST;
px4_gpio_init(gpio, arraySize(gpio));
// Configure SPI all interfaces GPIO & enable power.
stm32_spiinitialize();
// Check if button is held. If so go into gps passthrough mode
if (stm32_gpioread(GPIO_BTN_SAFETY)) {
rgb_led(128, 128, 128, 10);
stm32_configgpio(GPIO_USART1_TX_GPIO);
stm32_configgpio(GPIO_USART1_RX_GPIO);
stm32_configgpio(GPIO_USART2_TX_GPIO);
stm32_configgpio(GPIO_USART2_RX_GPIO);
while (1) {
watchdog_pet();
stm32_gpiowrite(GPIO_USART2_TX_GPIO, stm32_gpioread(GPIO_USART1_RX_GPIO));
stm32_gpiowrite(GPIO_USART1_TX_GPIO, stm32_gpioread(GPIO_USART2_RX_GPIO));
}
}
}
/****************************************************************************
* Name: board_app_initialize
*
* Description:
* Perform application specific initialization. This function is never
* called directly from application code, but only indirectly via the
* (non-standard) boardctl() interface using the command BOARDIOC_INIT.
*
* Input Parameters:
* arg - The boardctl() argument is passed to the board_app_initialize()
* implementation without modification. The argument has no
* meaning to NuttX; the meaning of the argument is a contract
* between the board-specific initalization logic and the the
* matching application logic. The value cold be such things as a
* mode enumeration value, a set of DIP switch switch settings, a
* pointer to configuration data read from a file or serial FLASH,
* or whatever you would like to do with it. Every implementation
* should accept zero/NULL as a default configuration.
*
* Returned Value:
* Zero (OK) is returned on success; a negated errno value is returned on
* any failure to indicate the nature of the failure.
*
****************************************************************************/
__EXPORT int board_app_initialize(uintptr_t arg)
{
px4_platform_init();
#if defined(SERIAL_HAVE_RXDMA)
// set up the serial DMA polling at 1ms intervals for received bytes that have not triggered a DMA event.
static struct hrt_call serial_dma_call;
hrt_call_every(&serial_dma_call, 1000, 1000, (hrt_callout)stm32_serial_dma_poll, NULL);
#endif
#if defined(FLASH_BASED_PARAMS)
static sector_descriptor_t params_sector_map[] = {
{2, 16 * 1024, 0x08008000},
{3, 16 * 1024, 0x0800C000},
{0, 0, 0},
};
/* Initialize the flashfs layer to use heap allocated memory */
int result = parameter_flashfs_init(params_sector_map, NULL, 0);
if (result != OK) {
syslog(LOG_ERR, "[boot] FAILED to init params in FLASH %d\n", result);
}
#endif // FLASH_BASED_PARAMS
/* Configure the HW based on the manifest */
//px4_platform_configure();
return OK;
}
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/****************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file led.c
*
* LED backend.
*/
#include <px4_platform_common/px4_config.h>
#include <stdbool.h>
#include "chip.h"
#include "stm32_gpio.h"
#include "board_config.h"
#include <nuttx/board.h>
#include <arch/board/board.h>
#include "led.h"
#define TMR_BASE STM32_TIM1_BASE
#define TMR_FREQUENCY STM32_APB2_TIM1_CLKIN
#define TMR_REG(o) (TMR_BASE+(o))
void rgb_led(int r, int g, int b, int freqs)
{
long fosc = TMR_FREQUENCY;
long prescale = 2048;
long p1s = fosc / prescale;
long p0p5s = p1s / 2;
uint16_t val;
static bool once = 0;
if (!once) {
once = 1;
/* Enabel Clock to Block */
modifyreg32(STM32_RCC_APB2ENR, 0, RCC_APB2ENR_TIM1EN);
/* Reload */
val = getreg16(TMR_REG(STM32_BTIM_EGR_OFFSET));
val |= ATIM_EGR_UG;
putreg16(val, TMR_REG(STM32_BTIM_EGR_OFFSET));
/* Set Prescaler STM32_TIM_SETCLOCK */
putreg16(prescale, TMR_REG(STM32_BTIM_PSC_OFFSET));
/* Enable STM32_TIM_SETMODE*/
putreg16(ATIM_CR1_CEN | ATIM_CR1_ARPE, TMR_REG(STM32_BTIM_CR1_OFFSET));
putreg16((ATIM_CCMR_MODE_PWM1 << ATIM_CCMR1_OC1M_SHIFT) | ATIM_CCMR1_OC1PE |
(ATIM_CCMR_MODE_PWM1 << ATIM_CCMR1_OC2M_SHIFT) | ATIM_CCMR1_OC2PE, TMR_REG(STM32_GTIM_CCMR1_OFFSET));
putreg16((ATIM_CCMR_MODE_PWM1 << ATIM_CCMR2_OC3M_SHIFT) | ATIM_CCMR2_OC3PE, TMR_REG(STM32_GTIM_CCMR2_OFFSET));
putreg16(ATIM_CCER_CC3E | ATIM_CCER_CC3P |
ATIM_CCER_CC2E | ATIM_CCER_CC2P |
ATIM_CCER_CC1E | ATIM_CCER_CC1P, TMR_REG(STM32_GTIM_CCER_OFFSET));
stm32_configgpio(GPIO_TIM1_CH1);
stm32_configgpio(GPIO_TIM1_CH2);
stm32_configgpio(GPIO_TIM1_CH3);
/* master output enable = on */
putreg16(ATIM_BDTR_MOE, (TMR_REG(STM32_ATIM_BDTR_OFFSET)));
}
long p = freqs == 0 ? p1s : p1s / freqs;
putreg32(p, TMR_REG(STM32_BTIM_ARR_OFFSET));
p = freqs == 0 ? p1s + 1 : p0p5s / freqs;
putreg32((r * p) / 255, TMR_REG(STM32_GTIM_CCR1_OFFSET));
putreg32((g * p) / 255, TMR_REG(STM32_GTIM_CCR2_OFFSET));
putreg32((b * p) / 255, TMR_REG(STM32_GTIM_CCR3_OFFSET));
val = getreg16(TMR_REG(STM32_BTIM_CR1_OFFSET));
if (freqs == 0) {
val &= ~ATIM_CR1_CEN;
} else {
val |= ATIM_CR1_CEN;
}
putreg16(val, TMR_REG(STM32_BTIM_CR1_OFFSET));
}
+37
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@@ -0,0 +1,37 @@
/****************************************************************************
*
* Copyright (C) 2015 PX4 Development Team. All rights reserved.
* Author: David Sidrane<david_s5@nscdg.com>
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
__BEGIN_DECLS
void rgb_led(int r, int g, int b, int freqs);
__END_DECLS
+44
View File
@@ -0,0 +1,44 @@
/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include <px4_arch/spi_hw_description.h>
#include <drivers/drv_sensor.h>
#include <nuttx/spi/spi.h>
constexpr px4_spi_bus_t px4_spi_buses[SPI_BUS_MAX_BUS_ITEMS] = {
initSPIBus(SPI::Bus::SPI1, {
initSPIDevice(DRV_IMU_DEVTYPE_ICM42688P, SPI::CS{GPIO::PortB, GPIO::Pin0}, SPI::DRDY{GPIO::PortB, GPIO::Pin1}),
}),
};
static constexpr bool unused = validateSPIConfig(px4_spi_buses);
@@ -0,0 +1,17 @@
# UAVCAN boot loadable Module ID
set(uavcanblid_sw_version_major ${PX4_VERSION_MAJOR})
set(uavcanblid_sw_version_minor ${PX4_VERSION_MINOR})
add_definitions(
-DAPP_VERSION_MAJOR=${uavcanblid_sw_version_major}
-DAPP_VERSION_MINOR=${uavcanblid_sw_version_minor}
)
set(uavcanblid_hw_version_major 0)
set(uavcanblid_hw_version_minor 84)
set(uavcanblid_name "\"org.ark.septentrio-gps\"")
add_definitions(
-DHW_UAVCAN_NAME=${uavcanblid_name}
-DHW_VERSION_MAJOR=${uavcanblid_hw_version_major}
-DHW_VERSION_MINOR=${uavcanblid_hw_version_minor}
)
+1 -1
View File
@@ -18,4 +18,4 @@ CONFIG_MODULES_UUV_POS_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -53,7 +53,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
-5
View File
@@ -1,21 +1,16 @@
CONFIG_DRIVERS_IRLOCK=n
CONFIG_MODULES_AIRSPEED_SELECTOR=n
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=n
CONFIG_MODULES_FLIGHT_MODE_MANAGER=n
CONFIG_MODULES_FW_ATT_CONTROL=n
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_FW_POS_CONTROL=n
CONFIG_MODULES_FW_RATE_CONTROL=n
CONFIG_MODULES_LANDING_TARGET_ESTIMATOR=n
CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
CONFIG_MODULES_MC_ATT_CONTROL=n
CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=n
CONFIG_MODULES_MC_POS_CONTROL=n
CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_UUV_ATT_CONTROL=n
CONFIG_MODULES_UUV_POS_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
+1 -6
View File
@@ -1,21 +1,16 @@
CONFIG_DRIVERS_IRLOCK=n
CONFIG_MODULES_AIRSPEED_SELECTOR=n
CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=n
CONFIG_MODULES_FLIGHT_MODE_MANAGER=n
CONFIG_MODULES_FW_ATT_CONTROL=n
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_FW_POS_CONTROL=n
CONFIG_MODULES_FW_RATE_CONTROL=n
CONFIG_MODULES_LANDING_TARGET_ESTIMATOR=n
CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
CONFIG_MODULES_MC_ATT_CONTROL=n
CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=n
CONFIG_MODULES_MC_POS_CONTROL=n
CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_UUV_ATT_CONTROL=n
CONFIG_MODULES_UUV_POS_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -13,4 +13,4 @@ CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1
View File
@@ -12,6 +12,7 @@ fi
if param compare -s ADC_ADS1115_EN 1
then
ads1115 start -X
board_adc start -n
else
board_adc start
fi
+1 -1
View File
@@ -13,4 +13,4 @@ CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -8,4 +8,4 @@ CONFIG_MODULES_MC_POS_CONTROL=n
CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -12,7 +12,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
CONFIG_MODULES_EKF2=y
CONFIG_EKF2_VERBOSE_STATUS=y
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
+5
View File
@@ -0,0 +1,5 @@
CONFIG_EKF2_AUX_GLOBAL_POSITION=n
CONFIG_EKF2_VERBOSE_STATUS=n
CONFIG_MODULES_EKF2=n
CONFIG_MODULES_SENSORS=y
CONFIG_BOARD_NOLOCKSTEP=y
+4
View File
@@ -1,4 +1,8 @@
uint64 timestamp # time since system start (microseconds)
float32 speed # [m/s] collective roll-off speed in body x-axis
bool closed_loop_speed_control # true if speed is controlled using estimator feedback, false if direct feed-forward
float32 yaw_rate # [rad/s] yaw rate
bool closed_loop_yaw_rate_control # true if yaw rate is controlled using gyroscope feedback, false if direct feed-forward
# TOPICS differential_drive_setpoint differential_drive_control_output
+6
View File
@@ -392,6 +392,12 @@ int BATT_SMBUS::get_startup_info()
uint16_t state_of_health;
ret |= _interface->read_word(BATT_SMBUS_STATE_OF_HEALTH, state_of_health);
/* ManufacturerAccess dummy command to init the ManufacturerBlockAccess routine
in the BQ40Zx0 and avoid timeout during LifetimeDataFlush.
test Sleep > 20 ms to give time to init the ManufacturerBlockAccess routine*/
ret |= _interface->write_word(BATT_SMBUS_MANUFACTURER_ACCESS, BATT_SMBUS_DEVICE_TYPE);
px4_usleep(30_ms);
if (!ret) {
_serial_number = serial_num;
_batt_startup_capacity = (uint16_t)((float)remaining_cap * _c_mult);
+1
View File
@@ -107,6 +107,7 @@ using namespace time_literals;
#define BATT_SMBUS_SECURITY_KEYS 0x0035
#define BATT_SMBUS_DEVICE_TYPE 0x0001
#define BATT_SMBUS_LIFETIME_FLUSH 0x002E
#define BATT_SMBUS_LIFETIME_BLOCK_ONE 0x0060
#define BATT_SMBUS_ENABLED_PROTECTIONS_A_ADDRESS 0x4938
@@ -113,7 +113,7 @@ CM8JL65::CM8JL65(const char *port, uint8_t rotation) :
_px4_rangefinder.set_max_distance(7.9f); // Datasheet: 8.0m
_px4_rangefinder.set_fov(0.0488692f);
_px4_rangefinder.set_device_type(DRV_DIST_DEVTYPE_CM8JL65);
_px4_rangefinder.set_rangefinder_type(distance_sensor_s::MAV_DISTANCE_SENSOR_LASER);
_px4_rangefinder.set_rangefinder_type(distance_sensor_s::MAV_DISTANCE_SENSOR_INFRARED);
}
CM8JL65::~CM8JL65()
+4 -4
View File
@@ -229,7 +229,7 @@ void PWMOut::update_params()
if (output_function >= (int)OutputFunction::Servo1
&& output_function <= (int)OutputFunction::ServoMax) { // Function got set to a servo
int32_t val = 1500;
PX4_INFO("Setting channel %i disarmed to %i", (int) val, i);
PX4_INFO("Setting channel %i disarmed to %i", i + 1, (int)val);
param_set(_mixing_output.disarmedParamHandle(i), &val);
// If the whole timer group was not set previously, then set the pwm rate to 50 Hz
@@ -250,7 +250,7 @@ void PWMOut::update_params()
if (param_get(handle, &tim_config) == 0 && tim_config == 400) {
tim_config = 50;
PX4_INFO("setting timer %i to %i Hz", timer, (int) tim_config);
PX4_INFO("Setting timer %i to %i Hz", timer, (int)tim_config);
param_set(handle, &tim_config);
}
}
@@ -261,10 +261,10 @@ void PWMOut::update_params()
if (output_function >= (int)OutputFunction::Motor1
&& output_function <= (int)OutputFunction::MotorMax) { // Function got set to a motor
int32_t val = 1100;
PX4_INFO("Setting channel %i minimum to %i", (int) val, i);
PX4_INFO("Setting channel %i minimum to %i", i + 1, (int)val);
param_set(_mixing_output.minParamHandle(i), &val);
val = 1900;
PX4_INFO("Setting channel %i maximum to %i", (int) val, i);
PX4_INFO("Setting channel %i maximum to %i", i + 1, (int)val);
param_set(_mixing_output.maxParamHandle(i), &val);
}
}
+4 -4
View File
@@ -705,7 +705,7 @@ void PX4IO::update_params()
if (output_function >= (int)OutputFunction::Servo1
&& output_function <= (int)OutputFunction::ServoMax) { // Function got set to a servo
int32_t val = 1500;
PX4_INFO("Setting channel %i disarmed to %i", (int) val, i);
PX4_INFO("Setting channel %i disarmed to %i", i + 1, (int)val);
param_set(_mixing_output.disarmedParamHandle(i), &val);
// If the whole timer group was not set previously, then set the pwm rate to 50 Hz
@@ -726,7 +726,7 @@ void PX4IO::update_params()
if (param_get(handle, &tim_config) == 0 && tim_config == 400) {
tim_config = 50;
PX4_INFO("setting timer %i to %i Hz", timer, (int) tim_config);
PX4_INFO("Setting timer %i to %i Hz", timer, (int)tim_config);
param_set(handle, &tim_config);
}
}
@@ -737,10 +737,10 @@ void PX4IO::update_params()
if (output_function >= (int)OutputFunction::Motor1
&& output_function <= (int)OutputFunction::MotorMax) { // Function got set to a motor
int32_t val = 1100;
PX4_INFO("Setting channel %i minimum to %i", (int) val, i);
PX4_INFO("Setting channel %i minimum to %i", i + 1, (int)val);
param_set(_mixing_output.minParamHandle(i), &val);
val = 1900;
PX4_INFO("Setting channel %i maximum to %i", (int) val, i);
PX4_INFO("Setting channel %i maximum to %i", i + 1, (int)val);
param_set(_mixing_output.maxParamHandle(i), &val);
}
}
@@ -189,7 +189,9 @@ param_import_callback(bson_decoder_t decoder, bson_node_t node)
return 0;
}
param_modify_on_import(node);
if (param_modify_on_import(node) == param_modify_on_import_ret::PARAM_SKIP_IMPORT) {
return 1;
}
/*
* Find the parameter this node represents. If we don't know it,
+4 -4
View File
@@ -40,7 +40,7 @@
#include <lib/parameters/param.h>
#include <lib/mathlib/mathlib.h>
bool param_modify_on_import(bson_node_t node)
param_modify_on_import_ret param_modify_on_import(bson_node_t node)
{
// 2023-12-06: translate and invert FW_ARSP_MODE-> FW_USE_AIRSPD
{
@@ -54,7 +54,7 @@ bool param_modify_on_import(bson_node_t node)
strcpy(node->name, "FW_USE_AIRSPD");
PX4_INFO("copying and inverting %s -> %s", "FW_ARSP_MODE", "FW_USE_AIRSPD");
return true;
return param_modify_on_import_ret::PARAM_MODIFIED;
}
}
@@ -69,9 +69,9 @@ bool param_modify_on_import(bson_node_t node)
}
return true;
return param_modify_on_import_ret::PARAM_MODIFIED;
}
}
return false;
return param_modify_on_import_ret::PARAM_NOT_MODIFIED;
}
+7 -1
View File
@@ -35,4 +35,10 @@
#include "tinybson/tinybson.h"
__EXPORT bool param_modify_on_import(bson_node_t node);
enum class param_modify_on_import_ret {
PARAM_SKIP_IMPORT = 0,
PARAM_NOT_MODIFIED = 1,
PARAM_MODIFIED = 2
};
__EXPORT param_modify_on_import_ret param_modify_on_import(bson_node_t node);
@@ -33,8 +33,8 @@
#include "param_translation.h"
bool param_modify_on_import(bson_node_t node)
param_modify_on_import_ret param_modify_on_import(bson_node_t node)
{
// don't modify params for unit tests
return false;
return param_modify_on_import_ret::PARAM_NOT_MODIFIED;
}
+4 -1
View File
@@ -1078,7 +1078,10 @@ param_import_callback(bson_decoder_t decoder, bson_node_t node)
return 0;
}
param_modify_on_import(node);
// if we do param_set() directly in the translation, set PARAM_SKIP_IMPORT as return value and return here
if (param_modify_on_import(node) == param_modify_on_import_ret::PARAM_SKIP_IMPORT) {
return 1;
}
// Find the parameter this node represents. If we don't know it, ignore the node.
param_t param = param_find_no_notification(node->name);
@@ -156,18 +156,18 @@ private:
#ifndef CONSTRAINED_FLASH
&_external_checks,
#endif
&_accelerometer_checks,
&_airspeed_checks,
//&_accelerometer_checks,
//&_airspeed_checks,
&_arm_permission_checks,
&_baro_checks,
//&_baro_checks,
&_cpu_resource_checks,
&_distance_sensor_checks,
&_esc_checks,
&_estimator_checks,
&_failure_detector_checks,
&_gyro_checks,
&_imu_consistency_checks,
&_magnetometer_checks,
//&_gyro_checks,
//&_imu_consistency_checks,
//&_magnetometer_checks,
&_manual_control_checks,
&_home_position_checks,
&_mission_checks,
@@ -99,7 +99,7 @@ void EstimatorChecks::checkAndReport(const Context &context, Report &reporter)
}
}
if (missing_data && _param_sys_mc_est_group.get() == 2) {
if (missing_data && _param_sys_mc_est_group.get() == 2 && false) {
/* EVENT
*/
reporter.armingCheckFailure(required_groups, health_component_t::local_position_estimate,
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2023 PX4 Development Team. All rights reserved.
# Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -31,17 +31,22 @@
#
############################################################################
add_subdirectory(DifferentialDriveControl)
add_subdirectory(DifferentialDriveGuidance)
add_subdirectory(DifferentialDriveKinematics)
px4_add_module(
MODULE modules__differential_drive_control
MAIN differential_drive_control
MODULE modules__differential_drive
MAIN differential_drive
SRCS
DifferentialDriveControl.cpp
DifferentialDriveControl.hpp
DifferentialDrive.cpp
DifferentialDrive.hpp
DEPENDS
DifferentialDriveControl
DifferentialDriveGuidance
DifferentialDriveKinematics
px4_work_queue
modules__control_allocator # for parameter CA_R_REV
MODULE_CONFIG
module.yaml
)
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -31,38 +31,37 @@
*
****************************************************************************/
#include "DifferentialDriveControl.hpp"
#include "DifferentialDrive.hpp"
using namespace time_literals;
using namespace matrix;
namespace differential_drive_control
{
DifferentialDriveControl::DifferentialDriveControl() :
DifferentialDrive::DifferentialDrive() :
ModuleParams(nullptr),
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::rate_ctrl)
{
updateParams();
}
bool DifferentialDriveControl::init()
bool DifferentialDrive::init()
{
ScheduleOnInterval(10_ms); // 100 Hz
return true;
}
void DifferentialDriveControl::updateParams()
void DifferentialDrive::updateParams()
{
ModuleParams::updateParams();
_max_speed = _param_rdd_max_wheel_speed.get() * _param_rdd_wheel_radius.get();
_max_angular_velocity = _max_speed / (_param_rdd_wheel_base.get() / 2.f);
_differential_drive_kinematics.setWheelBase(_param_rdd_wheel_base.get());
_max_speed = _param_rdd_wheel_speed.get() * _param_rdd_wheel_radius.get();
_differential_drive_guidance.setMaxSpeed(_max_speed);
_differential_drive_kinematics.setMaxSpeed(_max_speed);
_max_angular_velocity = _max_speed / (_param_rdd_wheel_base.get() / 2.f);
_differential_drive_guidance.setMaxAngularVelocity(_max_angular_velocity);
_differential_drive_kinematics.setMaxAngularVelocity(_max_angular_velocity);
}
void DifferentialDriveControl::Run()
void DifferentialDrive::Run()
{
if (should_exit()) {
ScheduleClear();
@@ -70,20 +69,32 @@ void DifferentialDriveControl::Run()
}
hrt_abstime now = hrt_absolute_time();
const float dt = math::min((now - _time_stamp_last), 5000_ms) / 1e6f;
_time_stamp_last = now;
if (_parameter_update_sub.updated()) {
parameter_update_s pupdate;
_parameter_update_sub.copy(&pupdate);
parameter_update_s parameter_update;
_parameter_update_sub.copy(&parameter_update);
updateParams();
}
if (_vehicle_control_mode_sub.updated()) {
vehicle_control_mode_s vehicle_control_mode;
vehicle_control_mode_s vehicle_control_mode{};
if (_vehicle_control_mode_sub.copy(&vehicle_control_mode)) {
_armed = vehicle_control_mode.flag_armed;
_manual_driving = vehicle_control_mode.flag_control_manual_enabled; // change this when more modes are supported
_manual_driving = vehicle_control_mode.flag_control_manual_enabled;
_mission_driving = vehicle_control_mode.flag_control_auto_enabled;
}
}
if (_vehicle_status_sub.updated()) {
vehicle_status_s vehicle_status{};
if (_vehicle_status_sub.copy(&vehicle_status)) {
const bool armed = (vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED);
const bool spooled_up = armed && (hrt_elapsed_time(&vehicle_status.armed_time) > _param_com_spoolup_time.get() * 1_s);
_differential_drive_kinematics.setArmed(spooled_up);
_acro_driving = (vehicle_status.nav_state == vehicle_status_s::NAVIGATION_STATE_ACRO);
}
}
@@ -94,43 +105,42 @@ void DifferentialDriveControl::Run()
manual_control_setpoint_s manual_control_setpoint{};
if (_manual_control_setpoint_sub.copy(&manual_control_setpoint)) {
_differential_drive_setpoint.timestamp = now;
_differential_drive_setpoint.speed = manual_control_setpoint.throttle * _param_rdd_speed_scale.get() * _max_speed;
_differential_drive_setpoint.yaw_rate = manual_control_setpoint.roll * _param_rdd_ang_velocity_scale.get() *
_max_angular_velocity;
_differential_drive_setpoint_pub.publish(_differential_drive_setpoint);
differential_drive_setpoint_s setpoint{};
setpoint.speed = manual_control_setpoint.throttle * math::max(0.f, _param_rdd_speed_scale.get()) * _max_speed;
setpoint.yaw_rate = manual_control_setpoint.roll * _param_rdd_ang_velocity_scale.get() * _max_angular_velocity;
// if acro mode, we activate the yaw rate control
if (_acro_driving) {
setpoint.closed_loop_speed_control = false;
setpoint.closed_loop_yaw_rate_control = true;
} else {
setpoint.closed_loop_speed_control = false;
setpoint.closed_loop_yaw_rate_control = false;
}
setpoint.timestamp = now;
_differential_drive_setpoint_pub.publish(setpoint);
}
}
} else if (_mission_driving) {
// Mission mode
// directly receive setpoints from the guidance library
_differential_drive_guidance.computeGuidance(
_differential_drive_control.getVehicleYaw(),
_differential_drive_control.getVehicleBodyYawRate(),
dt
);
}
_differential_drive_setpoint_sub.update(&_differential_drive_setpoint);
// publish data to actuator_motors (output module)
// get the wheel speeds from the inverse kinematics class (DifferentialDriveKinematics)
Vector2f wheel_speeds = _differential_drive_kinematics.computeInverseKinematics(
_differential_drive_setpoint.speed,
_differential_drive_setpoint.yaw_rate);
// Check if max_angular_wheel_speed is zero
const bool setpoint_timeout = (_differential_drive_setpoint.timestamp + 100_ms) < now;
const bool valid_max_speed = _param_rdd_speed_scale.get() > FLT_EPSILON;
if (!_armed || setpoint_timeout || !valid_max_speed) {
wheel_speeds = {}; // stop
}
wheel_speeds = matrix::constrain(wheel_speeds, -1.f, 1.f);
actuator_motors_s actuator_motors{};
actuator_motors.reversible_flags = _param_r_rev.get(); // should be 3 see rc.rover_differential_defaults
wheel_speeds.copyTo(actuator_motors.control);
actuator_motors.timestamp = now;
_actuator_motors_pub.publish(actuator_motors);
_differential_drive_control.control(dt);
_differential_drive_kinematics.allocate();
}
int DifferentialDriveControl::task_spawn(int argc, char *argv[])
int DifferentialDrive::task_spawn(int argc, char *argv[])
{
DifferentialDriveControl *instance = new DifferentialDriveControl();
DifferentialDrive *instance = new DifferentialDrive();
if (instance) {
_object.store(instance);
@@ -151,12 +161,12 @@ int DifferentialDriveControl::task_spawn(int argc, char *argv[])
return PX4_ERROR;
}
int DifferentialDriveControl::custom_command(int argc, char *argv[])
int DifferentialDrive::custom_command(int argc, char *argv[])
{
return print_usage("unknown command");
}
int DifferentialDriveControl::print_usage(const char *reason)
int DifferentialDrive::print_usage(const char *reason)
{
if (reason) {
PX4_ERR("%s\n", reason);
@@ -168,15 +178,13 @@ int DifferentialDriveControl::print_usage(const char *reason)
Rover Differential Drive controller.
)DESCR_STR");
PRINT_MODULE_USAGE_NAME("differential_drive_control", "controller");
PRINT_MODULE_USAGE_NAME("differential_drive", "controller");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
return 0;
}
extern "C" __EXPORT int differential_drive_control_main(int argc, char *argv[])
extern "C" __EXPORT int differential_drive_main(int argc, char *argv[])
{
return DifferentialDriveControl::main(argc, argv);
return DifferentialDrive::main(argc, argv);
}
} // namespace differential_drive_control
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -33,41 +33,31 @@
#pragma once
// PX4 includes
#include <px4_platform_common/px4_config.h>
#include <px4_platform_common/defines.h>
#include <px4_platform_common/module.h>
#include <px4_platform_common/module_params.h>
#include <px4_platform_common/px4_work_queue/ScheduledWorkItem.hpp>
// uORB includes
#include <uORB/topics/actuator_outputs.h>
#include <uORB/topics/actuator_motors.h>
#include <uORB/PublicationMulti.hpp>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionMultiArray.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/vehicle_status.h>
// Standard library includes
#include <math.h>
#include "DifferentialDriveControl/DifferentialDriveControl.hpp"
#include "DifferentialDriveGuidance/DifferentialDriveGuidance.hpp"
#include "DifferentialDriveKinematics/DifferentialDriveKinematics.hpp"
// Local includes
#include <DifferentialDriveKinematics.hpp>
using namespace time_literals;
namespace differential_drive_control
{
class DifferentialDriveControl : public ModuleBase<DifferentialDriveControl>, public ModuleParams,
class DifferentialDrive : public ModuleBase<DifferentialDrive>, public ModuleParams,
public px4::ScheduledWorkItem
{
public:
DifferentialDriveControl();
~DifferentialDriveControl() override = default;
DifferentialDrive();
~DifferentialDrive() override = default;
/** @see ModuleBase */
static int task_spawn(int argc, char *argv[]);
@@ -85,32 +75,31 @@ protected:
private:
void Run() override;
uORB::Subscription _differential_drive_setpoint_sub{ORB_ID(differential_drive_setpoint)};
uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
uORB::Subscription _parameter_update_sub{ORB_ID(parameter_update)};
uORB::Subscription _vehicle_control_mode_sub{ORB_ID(vehicle_control_mode)};
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
uORB::PublicationMulti<actuator_motors_s> _actuator_motors_pub{ORB_ID(actuator_motors)};
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_setpoint_pub{ORB_ID(differential_drive_setpoint)};
differential_drive_setpoint_s _differential_drive_setpoint{};
DifferentialDriveKinematics _differential_drive_kinematics{};
bool _armed = false;
bool _manual_driving = false;
bool _mission_driving = false;
bool _acro_driving = false;
hrt_abstime _time_stamp_last{0}; /**< time stamp when task was last updated */
DifferentialDriveGuidance _differential_drive_guidance{this};
DifferentialDriveControl _differential_drive_control{this};
DifferentialDriveKinematics _differential_drive_kinematics{this};
float _max_speed{0.f};
float _max_angular_velocity{0.f};
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_SPEED_SCALE>) _param_rdd_speed_scale,
(ParamFloat<px4::params::RDD_ANG_SCALE>) _param_rdd_ang_velocity_scale,
(ParamFloat<px4::params::RDD_WHL_SPEED>) _param_rdd_max_wheel_speed,
(ParamFloat<px4::params::RDD_SPEED_SCALE>) _param_rdd_speed_scale,
(ParamFloat<px4::params::RDD_WHEEL_BASE>) _param_rdd_wheel_base,
(ParamFloat<px4::params::RDD_WHEEL_SPEED>) _param_rdd_wheel_speed,
(ParamFloat<px4::params::RDD_WHEEL_RADIUS>) _param_rdd_wheel_radius,
(ParamInt<px4::params::CA_R_REV>) _param_r_rev
(ParamFloat<px4::params::COM_SPOOLUP_TIME>) _param_com_spoolup_time
)
};
} // namespace differential_drive_control
@@ -0,0 +1,39 @@
############################################################################
#
# Copyright (c) 2024 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
px4_add_library(DifferentialDriveControl
DifferentialDriveControl.cpp
)
target_link_libraries(DifferentialDriveControl PUBLIC pid)
target_include_directories(DifferentialDriveControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
@@ -0,0 +1,109 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include "DifferentialDriveControl.hpp"
using namespace matrix;
DifferentialDriveControl::DifferentialDriveControl(ModuleParams *parent) : ModuleParams(parent)
{
pid_init(&_pid_angular_velocity, PID_MODE_DERIVATIV_NONE, 0.001f);
pid_init(&_pid_speed, PID_MODE_DERIVATIV_NONE, 0.001f);
}
void DifferentialDriveControl::updateParams()
{
ModuleParams::updateParams();
pid_set_parameters(&_pid_angular_velocity,
_param_rdd_p_gain_angular_velocity.get(), // Proportional gain
_param_rdd_i_gain_angular_velocity.get(), // Integral gain
0, // Derivative gain
20, // Integral limit
200); // Output limit
pid_set_parameters(&_pid_speed,
_param_rdd_p_gain_speed.get(), // Proportional gain
_param_rdd_i_gain_speed.get(), // Integral gain
0, // Derivative gain
2, // Integral limit
200); // Output limit
}
void DifferentialDriveControl::control(float dt)
{
if (_vehicle_angular_velocity_sub.updated()) {
vehicle_angular_velocity_s vehicle_angular_velocity{};
if (_vehicle_angular_velocity_sub.copy(&vehicle_angular_velocity)) {
_vehicle_body_yaw_rate = vehicle_angular_velocity.xyz[2];
}
}
if (_vehicle_attitude_sub.updated()) {
vehicle_attitude_s vehicle_attitude{};
if (_vehicle_attitude_sub.copy(&vehicle_attitude)) {
_vehicle_attitude_quaternion = Quatf(vehicle_attitude.q);
_vehicle_yaw = matrix::Eulerf(_vehicle_attitude_quaternion).psi();
}
}
if (_vehicle_local_position_sub.updated()) {
vehicle_local_position_s vehicle_local_position{};
if (_vehicle_local_position_sub.copy(&vehicle_local_position)) {
Vector3f velocity_in_local_frame(vehicle_local_position.vx, vehicle_local_position.vy, vehicle_local_position.vz);
Vector3f velocity_in_body_frame = _vehicle_attitude_quaternion.rotateVectorInverse(velocity_in_local_frame);
_vehicle_forward_speed = velocity_in_body_frame(0);
}
}
_differential_drive_setpoint_sub.update(&_differential_drive_setpoint);
// PID to reach setpoint using control_output
differential_drive_setpoint_s differential_drive_control_output = _differential_drive_setpoint;
if (_differential_drive_setpoint.closed_loop_speed_control) {
differential_drive_control_output.speed +=
pid_calculate(&_pid_speed, _differential_drive_setpoint.speed, _vehicle_forward_speed, 0, dt);
}
if (_differential_drive_setpoint.closed_loop_yaw_rate_control) {
differential_drive_control_output.yaw_rate +=
pid_calculate(&_pid_angular_velocity, _differential_drive_setpoint.yaw_rate, _vehicle_body_yaw_rate, 0, dt);
}
differential_drive_control_output.timestamp = hrt_absolute_time();
_differential_drive_control_output_pub.publish(differential_drive_control_output);
}
@@ -0,0 +1,91 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file DifferentialDriveControl.hpp
*
* Controller for heading rate and forward speed.
*/
#pragma once
#include <lib/pid/pid.h>
#include <matrix/matrix/math.hpp>
#include <px4_platform_common/module_params.h>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/vehicle_angular_velocity.h>
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/vehicle_local_position.h>
class DifferentialDriveControl : public ModuleParams
{
public:
DifferentialDriveControl(ModuleParams *parent);
~DifferentialDriveControl() = default;
void control(float dt);
float getVehicleBodyYawRate() const { return _vehicle_body_yaw_rate; }
float getVehicleYaw() const { return _vehicle_yaw; }
protected:
void updateParams() override;
private:
uORB::Subscription _differential_drive_setpoint_sub{ORB_ID(differential_drive_setpoint)};
uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
uORB::Subscription _vehicle_attitude_sub{ORB_ID(vehicle_attitude)};
uORB::Subscription _vehicle_local_position_sub{ORB_ID(vehicle_local_position)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_control_output_pub{ORB_ID(differential_drive_control_output)};
differential_drive_setpoint_s _differential_drive_setpoint{};
matrix::Quatf _vehicle_attitude_quaternion{};
float _vehicle_yaw{0.f};
// States
float _vehicle_body_yaw_rate{0.f};
float _vehicle_forward_speed{0.f};
PID_t _pid_angular_velocity; ///< The PID controller for yaw rate.
PID_t _pid_speed; ///< The PID controller for velocity.
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_P_SPEED>) _param_rdd_p_gain_speed,
(ParamFloat<px4::params::RDD_I_SPEED>) _param_rdd_i_gain_speed,
(ParamFloat<px4::params::RDD_P_ANG_VEL>) _param_rdd_p_gain_angular_velocity,
(ParamFloat<px4::params::RDD_I_ANG_VEL>) _param_rdd_i_gain_angular_velocity
)
};
@@ -0,0 +1,38 @@
############################################################################
#
# Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
# are met:
#
# 1. Redistributions of source code must retain the above copyright
# notice, this list of conditions and the following disclaimer.
# 2. Redistributions in binary form must reproduce the above copyright
# notice, this list of conditions and the following disclaimer in
# the documentation and/or other materials provided with the
# distribution.
# 3. Neither the name PX4 nor the names of its contributors may be
# used to endorse or promote products derived from this software
# without specific prior written permission.
#
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
px4_add_library(DifferentialDriveGuidance
DifferentialDriveGuidance.cpp
)
target_include_directories(DifferentialDriveGuidance PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
@@ -0,0 +1,138 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include "DifferentialDriveGuidance.hpp"
#include <mathlib/math/Limits.hpp>
using namespace matrix;
DifferentialDriveGuidance::DifferentialDriveGuidance(ModuleParams *parent) : ModuleParams(parent)
{
updateParams();
pid_init(&_heading_p_controller, PID_MODE_DERIVATIV_NONE, 0.001f);
}
void DifferentialDriveGuidance::computeGuidance(float yaw, float angular_velocity, float dt)
{
if (_position_setpoint_triplet_sub.updated()) {
_position_setpoint_triplet_sub.copy(&_position_setpoint_triplet);
}
if (_vehicle_global_position_sub.updated()) {
_vehicle_global_position_sub.copy(&_vehicle_global_position);
}
matrix::Vector2d global_position(_vehicle_global_position.lat, _vehicle_global_position.lon);
matrix::Vector2d current_waypoint(_position_setpoint_triplet.current.lat, _position_setpoint_triplet.current.lon);
matrix::Vector2d next_waypoint(_position_setpoint_triplet.next.lat, _position_setpoint_triplet.next.lon);
const float distance_to_next_wp = get_distance_to_next_waypoint(global_position(0), global_position(1),
current_waypoint(0),
current_waypoint(1));
float desired_heading = get_bearing_to_next_waypoint(global_position(0), global_position(1), current_waypoint(0),
current_waypoint(1));
float heading_error = matrix::wrap_pi(desired_heading - yaw);
if (_current_waypoint != current_waypoint) {
_currentState = GuidanceState::TURNING;
}
// Make rover stop when it arrives at the last waypoint instead of loitering and driving around weirdly.
if ((current_waypoint == next_waypoint) && distance_to_next_wp <= _param_nav_acc_rad.get()) {
_currentState = GuidanceState::GOAL_REACHED;
}
float desired_speed = 0.f;
switch (_currentState) {
case GuidanceState::TURNING:
desired_speed = 0.f;
if (fabsf(heading_error) < 0.05f) {
_currentState = GuidanceState::DRIVING;
}
break;
case GuidanceState::DRIVING: {
const float max_velocity = math::trajectory::computeMaxSpeedFromDistance(_param_rdd_max_jerk.get(),
_param_rdd_max_accel.get(), distance_to_next_wp, 0.0f);
_forwards_velocity_smoothing.updateDurations(max_velocity);
_forwards_velocity_smoothing.updateTraj(dt);
desired_speed = math::interpolate<float>(abs(heading_error), 0.1f, 0.8f,
_forwards_velocity_smoothing.getCurrentVelocity(), 0.0f);
break;
}
case GuidanceState::GOAL_REACHED:
// temporary till I find a better way to stop the vehicle
desired_speed = 0.f;
heading_error = 0.f;
angular_velocity = 0.f;
_desired_angular_velocity = 0.f;
break;
}
// Compute the desired angular velocity relative to the heading error, to steer the vehicle towards the next waypoint.
float angular_velocity_pid = pid_calculate(&_heading_p_controller, heading_error, angular_velocity, 0,
dt) + heading_error;
differential_drive_setpoint_s output{};
output.speed = math::constrain(desired_speed, -_max_speed, _max_speed);
output.yaw_rate = math::constrain(angular_velocity_pid, -_max_angular_velocity, _max_angular_velocity);
output.closed_loop_speed_control = output.closed_loop_yaw_rate_control = true;
output.timestamp = hrt_absolute_time();
_differential_drive_setpoint_pub.publish(output);
_current_waypoint = current_waypoint;
}
void DifferentialDriveGuidance::updateParams()
{
ModuleParams::updateParams();
pid_set_parameters(&_heading_p_controller,
_param_rdd_p_gain_heading.get(), // Proportional gain
0, // Integral gain
0, // Derivative gain
0, // Integral limit
200); // Output limit
_forwards_velocity_smoothing.setMaxJerk(_param_rdd_max_jerk.get());
_forwards_velocity_smoothing.setMaxAccel(_param_rdd_max_accel.get());
_forwards_velocity_smoothing.setMaxVel(_max_speed);
}
@@ -0,0 +1,140 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#pragma once
#include <px4_platform_common/module_params.h>
#include <matrix/matrix/math.hpp>
#include <matrix/math.hpp>
#include <mathlib/mathlib.h>
#include <lib/geo/geo.h>
#include <math.h>
#include <lib/motion_planning/PositionSmoothing.hpp>
#include <lib/motion_planning/VelocitySmoothing.hpp>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/position_setpoint_triplet.h>
#include <uORB/topics/vehicle_global_position.h>
#include <lib/pid/pid.h>
/**
* @brief Enum class for the different states of guidance.
*/
enum class GuidanceState {
TURNING, ///< The vehicle is currently turning.
DRIVING, ///< The vehicle is currently driving straight.
GOAL_REACHED ///< The vehicle has reached its goal.
};
/**
* @brief Class for differential drive guidance.
*/
class DifferentialDriveGuidance : public ModuleParams
{
public:
/**
* @brief Constructor for DifferentialDriveGuidance.
* @param parent The parent ModuleParams object.
*/
DifferentialDriveGuidance(ModuleParams *parent);
~DifferentialDriveGuidance() = default;
/**
* @brief Compute guidance for the vehicle.
* @param global_pos The global position of the vehicle in degrees.
* @param current_waypoint The current waypoint the vehicle is heading towards in degrees.
* @param next_waypoint The next waypoint the vehicle will head towards after reaching the current waypoint in degrees.
* @param vehicle_yaw The yaw orientation of the vehicle in radians.
* @param body_velocity The velocity of the vehicle in m/s.
* @param angular_velocity The angular velocity of the vehicle in rad/s.
* @param dt The time step in seconds.
*/
void computeGuidance(float yaw, float angular_velocity, float dt);
/**
* @brief Set the maximum speed for the vehicle.
* @param max_speed The maximum speed in m/s.
* @return The set maximum speed in m/s.
*/
float setMaxSpeed(float max_speed) { return _max_speed = max_speed; }
/**
* @brief Set the maximum angular velocity for the vehicle.
* @param max_angular_velocity The maximum angular velocity in rad/s.
* @return The set maximum angular velocity in rad/s.
*/
float setMaxAngularVelocity(float max_angular_velocity) { return _max_angular_velocity = max_angular_velocity; }
protected:
/**
* @brief Update the parameters of the module.
*/
void updateParams() override;
private:
uORB::Subscription _position_setpoint_triplet_sub{ORB_ID(position_setpoint_triplet)};
uORB::Subscription _vehicle_global_position_sub{ORB_ID(vehicle_global_position)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_setpoint_pub{ORB_ID(differential_drive_setpoint)};
position_setpoint_triplet_s _position_setpoint_triplet{};
vehicle_global_position_s _vehicle_global_position{};
GuidanceState _currentState; ///< The current state of guidance.
float _desired_angular_velocity; ///< The desired angular velocity.
float _max_speed; ///< The maximum speed.
float _max_angular_velocity; ///< The maximum angular velocity.
matrix::Vector2d _current_waypoint; ///< The current waypoint.
VelocitySmoothing _forwards_velocity_smoothing; ///< The velocity smoothing for forward motion.
PositionSmoothing _position_smoothing; ///< The position smoothing.
PID_t _heading_p_controller; ///< The PID controller for yaw rate.
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_P_HEADING>) _param_rdd_p_gain_heading,
(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad,
(ParamFloat<px4::params::RDD_MAX_JERK>) _param_rdd_max_jerk,
(ParamFloat<px4::params::RDD_MAX_ACCEL>) _param_rdd_max_accel
)
};
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2023 PX4 Development Team. All rights reserved.
# Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -37,4 +37,4 @@ px4_add_library(DifferentialDriveKinematics
target_include_directories(DifferentialDriveKinematics PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
px4_add_unit_gtest(SRC DifferentialDriveKinematicsTest.cpp LINKLIBS DifferentialDriveKinematics)
px4_add_functional_gtest(SRC DifferentialDriveKinematicsTest.cpp LINKLIBS DifferentialDriveKinematics)
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2023 PX4 Development Team. All rights reserved.
* Copyright (C) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -36,8 +36,38 @@
#include <mathlib/mathlib.h>
using namespace matrix;
using namespace time_literals;
matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float linear_velocity_x, float yaw_rate)
DifferentialDriveKinematics::DifferentialDriveKinematics(ModuleParams *parent) : ModuleParams(parent)
{}
void DifferentialDriveKinematics::allocate()
{
hrt_abstime now = hrt_absolute_time();
if (_differential_drive_control_output_sub.updated()) {
_differential_drive_control_output_sub.copy(&_differential_drive_control_output);
}
const bool setpoint_timeout = (_differential_drive_control_output.timestamp + 100_ms) < now;
Vector2f wheel_speeds =
computeInverseKinematics(_differential_drive_control_output.speed, _differential_drive_control_output.yaw_rate);
if (!_armed || setpoint_timeout) {
wheel_speeds = {}; // stop
}
wheel_speeds = matrix::constrain(wheel_speeds, -1.f, 1.f);
actuator_motors_s actuator_motors{};
actuator_motors.reversible_flags = _param_r_rev.get(); // should be 3 see rc.rover_differential_defaults
wheel_speeds.copyTo(actuator_motors.control);
actuator_motors.timestamp = now;
_actuator_motors_pub.publish(actuator_motors);
}
matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float linear_velocity_x, float yaw_rate) const
{
if (_max_speed < FLT_EPSILON) {
return Vector2f();
@@ -54,7 +84,7 @@ matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float lin
if (combined_velocity > _max_speed) {
float excess_velocity = fabsf(combined_velocity - _max_speed);
float adjusted_linear_velocity = fabsf(linear_velocity_x) - excess_velocity;
const float adjusted_linear_velocity = fabsf(linear_velocity_x) - excess_velocity;
gain = adjusted_linear_velocity / fabsf(linear_velocity_x);
}
@@ -65,4 +95,3 @@ matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float lin
return Vector2f(linear_velocity_x - rotational_velocity,
linear_velocity_x + rotational_velocity) / _max_speed;
}
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -34,6 +34,11 @@
#pragma once
#include <matrix/matrix/math.hpp>
#include <px4_platform_common/module_params.h>
#include <uORB/PublicationMulti.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/actuator_motors.h>
#include <uORB/topics/differential_drive_setpoint.h>
/**
* @brief Differential Drive Kinematics class for computing the kinematics of a differential drive robot.
@@ -41,10 +46,10 @@
* This class provides functions to set the wheel base and radius, and to compute the inverse kinematics
* given linear velocity and yaw rate.
*/
class DifferentialDriveKinematics
class DifferentialDriveKinematics : public ModuleParams
{
public:
DifferentialDriveKinematics() = default;
DifferentialDriveKinematics(ModuleParams *parent);
~DifferentialDriveKinematics() = default;
/**
@@ -68,6 +73,10 @@ public:
*/
void setMaxAngularVelocity(const float max_angular_velocity) { _max_angular_velocity = max_angular_velocity; };
void setArmed(const bool armed) { _armed = armed; };
void allocate();
/**
* @brief Computes the inverse kinematics for differential drive.
*
@@ -75,10 +84,20 @@ public:
* @param yaw_rate Yaw rate of the robot.
* @return matrix::Vector2f Motor velocities for the right and left motors.
*/
matrix::Vector2f computeInverseKinematics(float linear_velocity_x, float yaw_rate);
matrix::Vector2f computeInverseKinematics(float linear_velocity_x, float yaw_rate) const;
private:
uORB::Subscription _differential_drive_control_output_sub{ORB_ID(differential_drive_control_output)};
uORB::PublicationMulti<actuator_motors_s> _actuator_motors_pub{ORB_ID(actuator_motors)};
differential_drive_setpoint_s _differential_drive_control_output{};
bool _armed = false;
float _wheel_base{0.f};
float _max_speed{0.f};
float _max_angular_velocity{0.f};
DEFINE_PARAMETERS(
(ParamInt<px4::params::CA_R_REV>) _param_r_rev
)
};
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2023 PX4 Development Team. All rights reserved.
* Copyright (C) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
@@ -37,9 +37,14 @@
using namespace matrix;
TEST(DifferentialDriveKinematicsTest, AllZeroInputCase)
class DifferentialDriveKinematicsTest : public ::testing::Test
{
public:
DifferentialDriveKinematics kinematics{nullptr};
};
TEST_F(DifferentialDriveKinematicsTest, AllZeroInputCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -49,9 +54,8 @@ TEST(DifferentialDriveKinematicsTest, AllZeroInputCase)
}
TEST(DifferentialDriveKinematicsTest, InvalidParameterCase)
TEST_F(DifferentialDriveKinematicsTest, InvalidParameterCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(0.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -61,9 +65,8 @@ TEST(DifferentialDriveKinematicsTest, InvalidParameterCase)
}
TEST(DifferentialDriveKinematicsTest, UnitCase)
TEST_F(DifferentialDriveKinematicsTest, UnitCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -73,9 +76,8 @@ TEST(DifferentialDriveKinematicsTest, UnitCase)
}
TEST(DifferentialDriveKinematicsTest, UnitSaturationCase)
TEST_F(DifferentialDriveKinematicsTest, UnitSaturationCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -85,9 +87,8 @@ TEST(DifferentialDriveKinematicsTest, UnitSaturationCase)
}
TEST(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
TEST_F(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -96,9 +97,8 @@ TEST(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
EXPECT_EQ(kinematics.computeInverseKinematics(-1.f, 1.f), Vector2f(-1, 0));
}
TEST(DifferentialDriveKinematicsTest, RandomCase)
TEST_F(DifferentialDriveKinematicsTest, RandomCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(2.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -107,9 +107,8 @@ TEST(DifferentialDriveKinematicsTest, RandomCase)
EXPECT_EQ(kinematics.computeInverseKinematics(0.5f, 0.7f), Vector2f(-0.4f, 1.0f));
}
TEST(DifferentialDriveKinematicsTest, RotateInPlaceCase)
TEST_F(DifferentialDriveKinematicsTest, RotateInPlaceCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -118,9 +117,8 @@ TEST(DifferentialDriveKinematicsTest, RotateInPlaceCase)
EXPECT_EQ(kinematics.computeInverseKinematics(0.f, 1.f), Vector2f(-0.5f, 0.5f));
}
TEST(DifferentialDriveKinematicsTest, StraightMovementCase)
TEST_F(DifferentialDriveKinematicsTest, StraightMovementCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -129,9 +127,8 @@ TEST(DifferentialDriveKinematicsTest, StraightMovementCase)
EXPECT_EQ(kinematics.computeInverseKinematics(1.f, 0.f), Vector2f(1.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MinInputValuesCase)
TEST_F(DifferentialDriveKinematicsTest, MinInputValuesCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(FLT_MIN);
kinematics.setMaxSpeed(FLT_MIN);
kinematics.setMaxAngularVelocity(FLT_MIN);
@@ -140,9 +137,8 @@ TEST(DifferentialDriveKinematicsTest, MinInputValuesCase)
EXPECT_EQ(kinematics.computeInverseKinematics(FLT_MIN, FLT_MIN), Vector2f(0.f, 0.f));
}
TEST(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
TEST_F(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -151,9 +147,8 @@ TEST(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
EXPECT_EQ(kinematics.computeInverseKinematics(10.f, 10.f), Vector2f(0.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
TEST_F(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -162,9 +157,8 @@ TEST(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
EXPECT_EQ(kinematics.computeInverseKinematics(10.f, 0.f), Vector2f(1.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MaxAngularCase)
TEST_F(DifferentialDriveKinematicsTest, MaxAngularCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(2.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -1,5 +1,5 @@
menuconfig MODULES_DIFFERENTIAL_DRIVE_CONTROL
bool "differential_drive_control"
menuconfig MODULES_DIFFERENTIAL_DRIVE
bool "differential_drive"
default n
depends on MODULES_CONTROL_ALLOCATOR
---help---
+122
View File
@@ -0,0 +1,122 @@
module_name: Differential Drive
parameters:
- group: Rover Differential Drive
definitions:
RDD_WHEEL_BASE:
description:
short: Wheel base
long: Distance from the center of the right wheel to the center of the left wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.5
RDD_WHEEL_RADIUS:
description:
short: Wheel radius
long: Size of the wheel, half the diameter of the wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.1
RDD_SPEED_SCALE:
description:
short: Manual speed scale
type: float
min: 0
max: 1
increment: 0.01
decimal: 2
default: 1
RDD_ANG_SCALE:
description:
short: Manual angular velocity scale
type: float
min: 0
max: 1
increment: 0.01
decimal: 2
default: 1
RDD_WHEEL_SPEED:
description:
short: Maximum wheel speed
type: float
unit: rad/s
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.3
RDD_P_HEADING:
description:
short: Proportional gain for heading controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_P_SPEED:
description:
short: Proportional gain for speed controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_I_SPEED:
description:
short: Integral gain for ground speed controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0
RDD_P_ANG_VEL:
description:
short: Proportional gain for angular velocity controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_I_ANG_VEL:
description:
short: Integral gain for angular velocity controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0
RDD_MAX_JERK:
description:
short: Maximum jerk
long: Limit for forwards acc/deceleration change.
type: float
unit: m/s^3
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.5
RDD_MAX_ACCEL:
description:
short: Maximum acceleration
long: Maximum acceleration is used to limit the acceleration of the rover
type: float
unit: m/s^2
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.5
@@ -1,55 +0,0 @@
module_name: Differential Drive Control
parameters:
- group: Rover Differential Drive
definitions:
RDD_WHEEL_BASE:
description:
short: Wheel base
long: Distance from the center of the right wheel to the center of the left wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.5
RDD_WHEEL_RADIUS:
description:
short: Wheel radius
long: Size of the wheel, half the diameter of the wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.1
RDD_SPEED_SCALE:
description:
short: Manual speed scale
type: float
min: 0
max: 1.0
increment: 0.01
decimal: 2
default: 1.0
RDD_ANG_SCALE:
description:
short: Manual angular velocity scale
type: float
min: 0
max: 1.0
increment: 0.01
decimal: 2
default: 1.0
RDD_WHL_SPEED:
description:
short: Maximum wheel speed
type: float
unit: rad/s
min: 0
max: 100
increment: 0.01
decimal: 2
default: 10
+4 -1
View File
@@ -80,8 +80,11 @@ void Ekf::controlGpsFusion(const imuSample &imu_delayed)
}
}
if (_pos_ref.isInitialized()) {
updateGnssPos(gnss_sample, _aid_src_gnss_pos);
}
updateGnssVel(gnss_sample, _aid_src_gnss_vel);
updateGnssPos(gnss_sample, _aid_src_gnss_pos);
} else if (_control_status.flags.gps) {
if (!isNewestSampleRecent(_time_last_gps_buffer_push, _params.reset_timeout_max)) {
@@ -175,7 +175,7 @@ def run(logfile):
res = optimize.minimize(J, x0, method='nelder-mead', options={'disp': True})
# Convert results to parameters
g = 9.81
g = 9.80665
pcoef_xn = res.x[0] * g
pcoef_xp = res.x[1] * g
pcoef_yn = res.x[2] * g
@@ -281,6 +281,12 @@ void FlightTaskAuto::_prepareLandSetpoints()
sticks_xy.setZero();
}
// If ground distance estimate valid (distance sensor) during nudging then limit horizontal speed
if (PX4_ISFINITE(_dist_to_bottom)) {
// Below 50cm no horizontal speed, above allow per meter altitude 0.5m/s speed
max_speed = math::max(0.f, math::min(max_speed, (_dist_to_bottom - .5f) * .5f));
}
_stick_acceleration_xy.setVelocityConstraint(max_speed);
_stick_acceleration_xy.generateSetpoints(sticks_xy, _yaw, _land_heading, _position,
_velocity_setpoint_feedback.xy(), _deltatime);
@@ -803,8 +809,8 @@ void FlightTaskAuto::_updateTrajConstraints()
if (_is_emergency_braking_active) {
// When initializing with large velocity, allow 1g of
// acceleration in 1s on all axes for fast braking
_position_smoothing.setMaxAcceleration({9.81f, 9.81f, 9.81f});
_position_smoothing.setMaxJerk(9.81f);
_position_smoothing.setMaxAcceleration({CONSTANTS_ONE_G, CONSTANTS_ONE_G, CONSTANTS_ONE_G});
_position_smoothing.setMaxJerk(CONSTANTS_ONE_G);
// If the current velocity is beyond the usual constraints, tell
// the controller to exceptionally increase its saturations to avoid
@@ -510,18 +510,38 @@ float FixedwingPositionControl::getCorrectedNpfgRollSetpoint()
{
// Scale the npfg output to zero if npfg is not certain for correct output
float new_roll_setpoint(_npfg.getRollSetpoint());
const float can_run_factor(_npfg.canRun(_local_pos, _wind_valid));
const float can_run_factor(constrain(_npfg.canRun(_local_pos, _wind_valid), 0.f, 1.f));
if ((1.f - can_run_factor) < FLT_EPSILON) {
// If the npfg was not running before, reset the user warning variables.
hrt_abstime now{hrt_absolute_time()};
if ((now - _time_since_last_npfg_call) > 2_s) {
_need_report_npfg_uncertain_condition = true;
_time_since_first_reduced_roll = 0U;
}
if (((1.f - can_run_factor) > FLT_EPSILON) && _need_report_npfg_uncertain_condition) {
_need_report_npfg_uncertain_condition = false;
events::send(events::ID("npfg_roll_command_uncertain"), events::Log::Warning,
"Roll command reduced due to uncertain velocity/wind estimates!");
// Warn the user when the scale is less than 90% for at least 2 seconds.
if ((1.f - can_run_factor) < 0.1f) {
_need_report_npfg_uncertain_condition = true;
_time_since_first_reduced_roll = 0U;
} else if (_need_report_npfg_uncertain_condition) {
if (_time_since_first_reduced_roll == 0U) {
_time_since_first_reduced_roll = hrt_absolute_time();
}
if ((now - _time_since_first_reduced_roll) > 2_s) {
_need_report_npfg_uncertain_condition = false;
events::send(events::ID("npfg_roll_command_uncertain"), events::Log::Warning,
"Roll command reduced due to uncertain velocity/wind estimates!");
}
} else {
// Nothing to do, already reported.
}
_time_since_last_npfg_call = now;
return can_run_factor * (new_roll_setpoint);
}
@@ -1368,7 +1388,7 @@ FixedwingPositionControl::control_auto_path(const float control_interval, const
0.0f;
navigatePathTangent(curr_pos_local, curr_wp_local, velocity_2d.normalized(), ground_speed, _wind_vel, curvature);
_att_sp.roll_body = _npfg.getRollSetpoint();
_att_sp.roll_body = getCorrectedNpfgRollSetpoint();
target_airspeed = _npfg.getAirspeedRef() / _eas2tas;
_att_sp.yaw_body = _yaw; // yaw is not controlled, so set setpoint to current yaw
@@ -414,6 +414,8 @@ private:
// nonlinear path following guidance - lateral-directional position control
NPFG _npfg;
bool _need_report_npfg_uncertain_condition{false}; ///< boolean if reporting of uncertain npfg output condition is needed
hrt_abstime _time_since_first_reduced_roll{0U}; ///< absolute time since start when entering reduced roll angle for the first time
hrt_abstime _time_since_last_npfg_call{0U}; ///< absolute time since start when the npfg reduced roll angle calculations was last performed
PerformanceModel _performance_model;
+1
View File
@@ -57,6 +57,7 @@ void LoggedTopics::add_default_topics()
add_topic("commander_state");
add_topic("config_overrides");
add_topic("cpuload");
add_optional_topic("differential_drive_control_output", 100);
add_optional_topic("differential_drive_setpoint", 100);
add_optional_topic("external_ins_attitude");
add_optional_topic("external_ins_global_position");
+22 -48
View File
@@ -928,16 +928,15 @@ MissionBlock::initialize()
_mission_item.origin = ORIGIN_ONBOARD;
}
void MissionBlock::setLoiterToAltMissionItem(mission_item_s &item, const DestinationPosition &dest, float loiter_radius,
HeadingMode heading_mode) const
void MissionBlock::setLoiterToAltMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp,
float loiter_radius) const
{
item.nav_cmd = NAV_CMD_LOITER_TO_ALT;
item.lat = dest.lat;
item.lon = dest.lon;
item.altitude = dest.alt;
item.lat = pos_yaw_sp.lat;
item.lon = pos_yaw_sp.lon;
item.altitude = pos_yaw_sp.alt;
item.altitude_is_relative = false;
item. yaw = setYawFromHeadingMode(dest, heading_mode);
item.yaw = pos_yaw_sp.yaw;
item.acceptance_radius = _navigator->get_acceptance_radius();
item.time_inside = 0.0f;
@@ -946,8 +945,8 @@ void MissionBlock::setLoiterToAltMissionItem(mission_item_s &item, const Destina
item.loiter_radius = loiter_radius;
}
void MissionBlock::setLoiterHoldMissionItem(mission_item_s &item, const DestinationPosition &dest, float loiter_time,
float loiter_radius, HeadingMode heading_mode) const
void MissionBlock::setLoiterHoldMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp,
float loiter_time, float loiter_radius) const
{
const bool autocontinue = (loiter_time > -FLT_EPSILON);
@@ -958,12 +957,12 @@ void MissionBlock::setLoiterHoldMissionItem(mission_item_s &item, const Destinat
item.nav_cmd = NAV_CMD_LOITER_UNLIMITED;
}
item.lat = dest.lat;
item.lon = dest.lon;
item.altitude = dest.alt;
item.lat = pos_yaw_sp.lat;
item.lon = pos_yaw_sp.lon;
item.altitude = pos_yaw_sp.alt;
item.altitude_is_relative = false;
item. yaw = setYawFromHeadingMode(dest, heading_mode);
item.yaw = NAN;
item.acceptance_radius = _navigator->get_acceptance_radius();
item.time_inside = math::max(loiter_time, 0.0f);
@@ -972,13 +971,12 @@ void MissionBlock::setLoiterHoldMissionItem(mission_item_s &item, const Destinat
item.loiter_radius = loiter_radius;
}
void MissionBlock::setMoveToPositionMissionItem(mission_item_s &item, const DestinationPosition &dest,
HeadingMode heading_mode) const
void MissionBlock::setMoveToPositionMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp) const
{
item.nav_cmd = NAV_CMD_WAYPOINT;
item.lat = dest.lat;
item.lon = dest.lon;
item.altitude = dest.alt;
item.lat = pos_yaw_sp.lat;
item.lon = pos_yaw_sp.lon;
item.altitude = pos_yaw_sp.alt;
item.altitude_is_relative = false;
item.autocontinue = true;
@@ -986,46 +984,22 @@ void MissionBlock::setMoveToPositionMissionItem(mission_item_s &item, const Dest
item.time_inside = 0.f;
item.origin = ORIGIN_ONBOARD;
item. yaw = setYawFromHeadingMode(dest, heading_mode);
item.yaw = pos_yaw_sp.yaw;
}
void MissionBlock::setLandMissionItem(mission_item_s &item, const DestinationPosition &dest,
HeadingMode heading_mode) const
void MissionBlock::setLandMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp) const
{
item.nav_cmd = NAV_CMD_LAND;
item.lat = dest.lat;
item.lon = dest.lon;
item.altitude = dest.alt;
if (heading_mode == HeadingMode::CURRENT_HEADING) {
item.yaw = _navigator->get_local_position()->heading;
} else {
item.yaw = dest.yaw;
}
item.lat = pos_yaw_sp.lat;
item.lon = pos_yaw_sp.lon;
item.altitude = pos_yaw_sp.alt;
item.yaw = pos_yaw_sp.yaw;
item.acceptance_radius = _navigator->get_acceptance_radius();
item.time_inside = 0.0f;
item.autocontinue = true;
item.origin = ORIGIN_ONBOARD;
}
float MissionBlock::setYawFromHeadingMode(const DestinationPosition &dest, HeadingMode heading_mode) const
{
float desired_yaw(_navigator->get_local_position()->heading);
if (heading_mode == HeadingMode::NAVIGATION_HEADING) {
desired_yaw = get_bearing_to_next_waypoint(_navigator->get_global_position()->lat,
_navigator->get_global_position()->lon, dest.lat, dest.lon);
} else if (heading_mode == HeadingMode::DESTINATION_HEADING) {
desired_yaw = dest.yaw;
}
return desired_yaw;
}
void MissionBlock::startPrecLand(uint16_t land_precision)
{
if (_mission_item.land_precision == 1) {
+5 -9
View File
@@ -205,18 +205,14 @@ protected:
*/
void set_vtol_transition_item(struct mission_item_s *item, const uint8_t new_mode);
void setLoiterToAltMissionItem(mission_item_s &item, const DestinationPosition &dest, float loiter_radius,
HeadingMode heading_mode) const;
void setLoiterToAltMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp, float loiter_radius) const;
void setLoiterHoldMissionItem(mission_item_s &item, const DestinationPosition &dest, float loiter_time,
float loiter_radius, HeadingMode heading_mode) const;
void setLoiterHoldMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp, float loiter_time,
float loiter_radius) const;
void setMoveToPositionMissionItem(mission_item_s &item, const DestinationPosition &dest,
HeadingMode heading_mode) const;
void setMoveToPositionMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp) const;
void setLandMissionItem(mission_item_s &item, const DestinationPosition &dest, HeadingMode heading_mode) const;
float setYawFromHeadingMode(const DestinationPosition &dest, HeadingMode heading_mode) const;
void setLandMissionItem(mission_item_s &item, const PositionYawSetpoint &pos_yaw_sp) const;
void startPrecLand(uint16_t land_precision);
+7 -7
View File
@@ -230,15 +230,15 @@ struct mission_fence_point_s {
};
/**
* @brief Return to launch position.
* Defines the position and landing yaw for the return to launch destination.
* @brief Position and yaw setpoint struct.
* Used in RTL state machine.
*
*/
struct DestinationPosition {
double lat; /**< latitude in WGS84 [rad].*/
double lon; /**< longitude in WGS84 [rad].*/
float alt; /**< altitude in MSL [m].*/
float yaw; /**< final yaw when landed [rad].*/
struct PositionYawSetpoint {
double lat; /**< latitude setpoint in WGS84 [rad].*/
double lon; /**< longitude setpoint in WGS84 [rad].*/
float alt; /**< altitude setpoint in MSL [m].*/
float yaw; /**< yaw setpoint [rad].*/
};
+8 -8
View File
@@ -297,7 +297,7 @@ void RTL::setRtlTypeAndDestination()
if (_param_rtl_type.get() != 2) {
// check the closest allowed destination.
DestinationType destination_type{DestinationType::DESTINATION_TYPE_HOME};
DestinationPosition rtl_position;
PositionYawSetpoint rtl_position;
float rtl_alt;
findRtlDestination(destination_type, rtl_position, rtl_alt);
@@ -333,7 +333,7 @@ void RTL::setRtlTypeAndDestination()
}
}
void RTL::findRtlDestination(DestinationType &destination_type, DestinationPosition &rtl_position, float &rtl_alt)
void RTL::findRtlDestination(DestinationType &destination_type, PositionYawSetpoint &rtl_position, float &rtl_alt)
{
// set destination to home per default, then check if other valid landing spot is closer
rtl_position.alt = _home_pos_sub.get().alt;
@@ -413,7 +413,7 @@ void RTL::findRtlDestination(DestinationType &destination_type, DestinationPosit
if (mission_safe_point.nav_cmd == NAV_CMD_RALLY_POINT && dist_to_home > MAX_DIST_FROM_HOME_FOR_LAND_APPROACHES) {
float dist{get_distance_to_next_waypoint(_global_pos_sub.get().lat, _global_pos_sub.get().lon, mission_safe_point.lat, mission_safe_point.lon)};
DestinationPosition safepoint_position;
PositionYawSetpoint safepoint_position;
setSafepointAsDestination(safepoint_position, mission_safe_point);
if (((dist + MIN_DIST_THRESHOLD) < min_dist) && (!vtol_in_fw_mode || (_param_rtl_approach_force.get() == 0)
@@ -435,7 +435,7 @@ void RTL::findRtlDestination(DestinationType &destination_type, DestinationPosit
}
}
void RTL::setLandPosAsDestination(DestinationPosition &rtl_position, mission_item_s &land_mission_item) const
void RTL::setLandPosAsDestination(PositionYawSetpoint &rtl_position, mission_item_s &land_mission_item) const
{
rtl_position.alt = land_mission_item.altitude_is_relative ? land_mission_item.altitude +
_home_pos_sub.get().alt : land_mission_item.altitude;
@@ -444,7 +444,7 @@ void RTL::setLandPosAsDestination(DestinationPosition &rtl_position, mission_ite
rtl_position.yaw = _home_pos_sub.get().yaw;
}
void RTL::setSafepointAsDestination(DestinationPosition &rtl_position,
void RTL::setSafepointAsDestination(PositionYawSetpoint &rtl_position,
const mission_item_s &mission_safe_point) const
{
// There is a safe point closer than home/mission landing
@@ -472,7 +472,7 @@ void RTL::setSafepointAsDestination(DestinationPosition &rtl_position,
}
}
float RTL::calculate_return_alt_from_cone_half_angle(const DestinationPosition &rtl_position,
float RTL::calculate_return_alt_from_cone_half_angle(const PositionYawSetpoint &rtl_position,
float cone_half_angle_deg) const
{
// horizontal distance to destination
@@ -576,7 +576,7 @@ bool RTL::hasMissionLandStart() const
return _mission_sub.get().land_start_index > 0;
}
bool RTL::hasVtolLandApproach(const DestinationPosition &rtl_position) const
bool RTL::hasVtolLandApproach(const PositionYawSetpoint &rtl_position) const
{
return readVtolLandApproaches(rtl_position).isAnyApproachValid();
}
@@ -611,7 +611,7 @@ loiter_point_s RTL::chooseBestLandingApproach(const land_approaches_s &vtol_land
}
}
land_approaches_s RTL::readVtolLandApproaches(DestinationPosition rtl_position) const
land_approaches_s RTL::readVtolLandApproaches(PositionYawSetpoint rtl_position) const
{
// go through all mission items in the rally point storage. If we find a mission item of type NAV_CMD_RALLY_POINT
+6 -6
View File
@@ -109,20 +109,20 @@ private:
* @brief Find RTL destination.
*
*/
void findRtlDestination(DestinationType &destination_type, DestinationPosition &rtl_position, float &rtl_alt);
void findRtlDestination(DestinationType &destination_type, PositionYawSetpoint &rtl_position, float &rtl_alt);
/**
* @brief Set the position of the land start marker in the planned mission as destination.
*
*/
void setLandPosAsDestination(DestinationPosition &rtl_position, mission_item_s &land_mission_item) const;
void setLandPosAsDestination(PositionYawSetpoint &rtl_position, mission_item_s &land_mission_item) const;
/**
* @brief Set the safepoint as destination.
*
* @param mission_safe_point is the mission safe point/rally point to set as destination.
*/
void setSafepointAsDestination(DestinationPosition &rtl_position, const mission_item_s &mission_safe_point) const;
void setSafepointAsDestination(PositionYawSetpoint &rtl_position, const mission_item_s &mission_safe_point) const;
/**
* @brief calculate return altitude from cone half angle
@@ -131,7 +131,7 @@ private:
* @param[in] cone_half_angle_deg half angle of the cone [deg]
* @return return altitude
*/
float calculate_return_alt_from_cone_half_angle(const DestinationPosition &rtl_position,
float calculate_return_alt_from_cone_half_angle(const PositionYawSetpoint &rtl_position,
float cone_half_angle_deg) const;
/**
@@ -152,7 +152,7 @@ private:
* @param[in] rtl_position landing position of the rtl
*
*/
land_approaches_s readVtolLandApproaches(DestinationPosition rtl_position) const;
land_approaches_s readVtolLandApproaches(PositionYawSetpoint rtl_position) const;
/**
* @brief Has VTOL land approach
@@ -162,7 +162,7 @@ private:
* @return true if home land approaches are defined for home position
* @return false otherwise
*/
bool hasVtolLandApproach(const DestinationPosition &rtl_position) const;
bool hasVtolLandApproach(const PositionYawSetpoint &rtl_position) const;
/**
* @brief Choose best landing approach
+28 -28
View File
@@ -122,7 +122,7 @@ void RtlDirect::on_active()
}
}
void RtlDirect::setRtlPosition(DestinationPosition rtl_position, loiter_point_s loiter_pos)
void RtlDirect::setRtlPosition(PositionYawSetpoint rtl_position, loiter_point_s loiter_pos)
{
_home_pos_sub.update();
@@ -178,41 +178,39 @@ void RtlDirect::set_rtl_item()
_global_pos_sub.get().lat, _global_pos_sub.get().lon);
const float loiter_altitude = math::min(_land_approach.height_m, _rtl_alt);
HeadingMode rtl_heading_mode = static_cast<HeadingMode>(_param_rtl_hdg_md.get());
if ((rtl_heading_mode == HeadingMode::NAVIGATION_HEADING) && (destination_dist < _param_rtl_min_dist.get())) {
rtl_heading_mode = HeadingMode::DESTINATION_HEADING;
}
const bool is_close_to_destination = destination_dist < _param_rtl_min_dist.get();
switch (_rtl_state) {
case RTLState::CLIMBING: {
DestinationPosition dest {
PositionYawSetpoint pos_yaw_sp {
.lat = _global_pos_sub.get().lat,
.lon = _global_pos_sub.get().lon,
.alt = _rtl_alt,
.yaw = _param_wv_en.get() ? NAN : _navigator->get_local_position()->heading,
};
setLoiterToAltMissionItem(_mission_item, dest, _navigator->get_loiter_radius(), HeadingMode::CURRENT_HEADING);
setLoiterToAltMissionItem(_mission_item, pos_yaw_sp, _navigator->get_loiter_radius());
_rtl_state = RTLState::MOVE_TO_LOITER;
break;
}
case RTLState::MOVE_TO_LOITER: {
DestinationPosition dest {
PositionYawSetpoint pos_yaw_sp {
.lat = _land_approach.lat,
.lon = _land_approach.lon,
.alt = _rtl_alt,
.yaw = _destination.yaw,
};
// For FW flight:set to LOITER_TIME (with 0s loiter time), such that the loiter (orbit) status
// can be displayed on groundstation and the WP is accepted once within loiter radius
if (_vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING) {
setLoiterHoldMissionItem(_mission_item, dest, 0.f, _land_approach.loiter_radius_m, rtl_heading_mode);
pos_yaw_sp.yaw = NAN;
setLoiterHoldMissionItem(_mission_item, pos_yaw_sp, 0.f, _land_approach.loiter_radius_m);
} else {
setMoveToPositionMissionItem(_mission_item, dest, rtl_heading_mode);
// already set final yaw if close to destination and weather vane is disabled
pos_yaw_sp.yaw = (is_close_to_destination && !_param_wv_en.get()) ? _destination.yaw : NAN;
setMoveToPositionMissionItem(_mission_item, pos_yaw_sp);
}
_rtl_state = RTLState::LOITER_DOWN;
@@ -221,14 +219,14 @@ void RtlDirect::set_rtl_item()
}
case RTLState::LOITER_DOWN: {
DestinationPosition dest{
PositionYawSetpoint pos_yaw_sp{
.lat = _land_approach.lat,
.lon = _land_approach.lon,
.alt = loiter_altitude,
.yaw = _destination.yaw,
.yaw = !_param_wv_en.get() ? _destination.yaw : NAN, // set final yaw if weather vane is disabled
};
setLoiterToAltMissionItem(_mission_item, dest, _land_approach.loiter_radius_m, rtl_heading_mode);
setLoiterToAltMissionItem(_mission_item, pos_yaw_sp, _land_approach.loiter_radius_m);
pos_sp_triplet->next.valid = true;
pos_sp_triplet->next.lat = _destination.lat;
@@ -248,15 +246,14 @@ void RtlDirect::set_rtl_item()
}
case RTLState::LOITER_HOLD: {
DestinationPosition dest {
PositionYawSetpoint pos_yaw_sp {
.lat = _land_approach.lat,
.lon = _land_approach.lon,
.alt = loiter_altitude,
.yaw = _destination.yaw,
.yaw = !_param_wv_en.get() ? _destination.yaw : NAN, // set final yaw if weather vane is disabled
};
setLoiterHoldMissionItem(_mission_item, dest, _param_rtl_land_delay.get(), _land_approach.loiter_radius_m,
rtl_heading_mode);
setLoiterHoldMissionItem(_mission_item, pos_yaw_sp, _param_rtl_land_delay.get(), _land_approach.loiter_radius_m);
if (_param_rtl_land_delay.get() < -FLT_EPSILON) {
mavlink_log_info(_navigator->get_mavlink_log_pub(), "RTL: completed, loitering\t");
@@ -276,10 +273,11 @@ void RtlDirect::set_rtl_item()
case RTLState::MOVE_TO_LAND: {
DestinationPosition dest{_destination};
dest.alt = loiter_altitude;
PositionYawSetpoint pos_yaw_sp{_destination};
pos_yaw_sp.alt = loiter_altitude;
pos_yaw_sp.yaw = NAN;
setMoveToPositionMissionItem(_mission_item, dest, rtl_heading_mode);
setMoveToPositionMissionItem(_mission_item, pos_yaw_sp);
// Prepare for transition
_mission_item.vtol_back_transition = true;
@@ -306,10 +304,11 @@ void RtlDirect::set_rtl_item()
}
case RTLState::MOVE_TO_LAND_HOVER: {
DestinationPosition dest{_destination};
dest.alt = loiter_altitude;
PositionYawSetpoint pos_yaw_sp{_destination};
pos_yaw_sp.alt = loiter_altitude;
pos_yaw_sp.yaw = !_param_wv_en.get() ? _destination.yaw : NAN; // set final yaw if weather vane is disabled
setMoveToPositionMissionItem(_mission_item, dest, rtl_heading_mode);
setMoveToPositionMissionItem(_mission_item, pos_yaw_sp);
_navigator->reset_position_setpoint(pos_sp_triplet->previous);
_rtl_state = RTLState::LAND;
@@ -318,8 +317,9 @@ void RtlDirect::set_rtl_item()
}
case RTLState::LAND: {
setLandMissionItem(_mission_item, _destination, rtl_heading_mode);
PositionYawSetpoint pos_yaw_sp{_destination};
pos_yaw_sp.yaw = !_param_wv_en.get() ? _destination.yaw : NAN; // set final yaw if weather vane is disabled
setLandMissionItem(_mission_item, pos_yaw_sp);
_mission_item.land_precision = _param_rtl_pld_md.get();
+6 -4
View File
@@ -99,7 +99,7 @@ public:
void setReturnAltMin(bool min) { _enforce_rtl_alt = min; }
void setRtlAlt(float alt) {_rtl_alt = alt;};
void setRtlPosition(DestinationPosition position, loiter_point_s loiter_pos);
void setRtlPosition(PositionYawSetpoint position, loiter_point_s loiter_pos);
private:
/**
@@ -179,7 +179,7 @@ private:
bool _enforce_rtl_alt{false};
bool _force_heading{false};
DestinationPosition _destination; ///< the RTL position to fly to
PositionYawSetpoint _destination; ///< the RTL position to fly to
loiter_point_s _land_approach;
float _rtl_alt{0.0f}; ///< AMSL altitude at which the vehicle should return to the home position
@@ -190,9 +190,11 @@ private:
(ParamFloat<px4::params::RTL_MIN_DIST>) _param_rtl_min_dist,
(ParamInt<px4::params::RTL_PLD_MD>) _param_rtl_pld_md,
(ParamFloat<px4::params::RTL_LOITER_RAD>) _param_rtl_loiter_rad,
(ParamInt<px4::params::RTL_HDG_MD>) _param_rtl_hdg_md,
(ParamFloat<px4::params::RTL_TIME_FACTOR>) _param_rtl_time_factor,
(ParamInt<px4::params::RTL_TIME_MARGIN>) _param_rtl_time_margin
(ParamInt<px4::params::RTL_TIME_MARGIN>) _param_rtl_time_margin,
// external params
(ParamBool<px4::params::WV_EN>) _param_wv_en
)
param_t _param_mpc_z_v_auto_up{PARAM_INVALID};
-12
View File
@@ -160,18 +160,6 @@ PARAM_DEFINE_INT32(RTL_PLD_MD, 0);
*/
PARAM_DEFINE_FLOAT(RTL_LOITER_RAD, 80.0f);
/**
* RTL heading mode
*
* Defines the heading behavior during RTL
*
* @value 0 Towards next waypoint.
* @value 1 Heading matches destination.
* @value 2 Use current heading.
* @group Return Mode
*/
PARAM_DEFINE_INT32(RTL_HDG_MD, 0);
/**
* RTL time estimate safety margin factor
*
+64 -25
View File
@@ -216,6 +216,15 @@ int GZBridge::init()
return PX4_ERROR;
}
// GPS: /world/$WORLD/model/$MODEL/link/base_link/sensor/navsat_sensor/navsat
std::string nav_sat_topic = "/world/" + _world_name + "/model/" + _model_name +
"/link/base_link/sensor/navsat_sensor/navsat";
if (!_node.Subscribe(nav_sat_topic, &GZBridge::navSatCallback, this)) {
PX4_ERR("failed to subscribe to %s", nav_sat_topic.c_str());
return PX4_ERROR;
}
if (!_mixing_interface_esc.init(_model_name)) {
PX4_ERR("failed to init ESC output");
return PX4_ERROR;
@@ -565,10 +574,6 @@ void GZBridge::poseInfoCallback(const gz::msgs::Pose_V &pose)
vehicle_angular_velocity_groundtruth.timestamp = hrt_absolute_time();
_angular_velocity_ground_truth_pub.publish(vehicle_angular_velocity_groundtruth);
if (!_pos_ref.isInitialized()) {
_pos_ref.initReference((double)_param_sim_home_lat.get(), (double)_param_sim_home_lon.get(), hrt_absolute_time());
}
vehicle_local_position_s local_position_groundtruth{};
#if defined(ENABLE_LOCKSTEP_SCHEDULER)
local_position_groundtruth.timestamp_sample = time_us;
@@ -595,31 +600,27 @@ void GZBridge::poseInfoCallback(const gz::msgs::Pose_V &pose)
local_position_groundtruth.heading = euler.psi();
local_position_groundtruth.ref_lat = _pos_ref.getProjectionReferenceLat(); // Reference point latitude in degrees
local_position_groundtruth.ref_lon = _pos_ref.getProjectionReferenceLon(); // Reference point longitude in degrees
local_position_groundtruth.ref_alt = _param_sim_home_alt.get();
local_position_groundtruth.ref_timestamp = _pos_ref.getProjectionReferenceTimestamp();
if (_pos_ref.isInitialized()) {
local_position_groundtruth.ref_lat = _pos_ref.getProjectionReferenceLat(); // Reference point latitude in degrees
local_position_groundtruth.ref_lon = _pos_ref.getProjectionReferenceLon(); // Reference point longitude in degrees
local_position_groundtruth.ref_alt = _alt_ref;
local_position_groundtruth.ref_timestamp = _pos_ref.getProjectionReferenceTimestamp();
local_position_groundtruth.xy_global = true;
local_position_groundtruth.z_global = true;
} else {
local_position_groundtruth.ref_lat = static_cast<double>(NAN);
local_position_groundtruth.ref_lon = static_cast<double>(NAN);
local_position_groundtruth.ref_alt = NAN;
local_position_groundtruth.ref_timestamp = 0;
local_position_groundtruth.xy_global = false;
local_position_groundtruth.z_global = false;
}
local_position_groundtruth.timestamp = hrt_absolute_time();
_lpos_ground_truth_pub.publish(local_position_groundtruth);
if (_pos_ref.isInitialized()) {
// publish position groundtruth
vehicle_global_position_s global_position_groundtruth{};
#if defined(ENABLE_LOCKSTEP_SCHEDULER)
global_position_groundtruth.timestamp_sample = time_us;
#else
global_position_groundtruth.timestamp_sample = hrt_absolute_time();
#endif
_pos_ref.reproject(local_position_groundtruth.x, local_position_groundtruth.y,
global_position_groundtruth.lat, global_position_groundtruth.lon);
global_position_groundtruth.alt = _param_sim_home_alt.get() - static_cast<float>(position(2));
global_position_groundtruth.timestamp = hrt_absolute_time();
_gpos_ground_truth_pub.publish(global_position_groundtruth);
}
pthread_mutex_unlock(&_node_mutex);
return;
}
@@ -704,6 +705,44 @@ void GZBridge::odometryCallback(const gz::msgs::OdometryWithCovariance &odometry
pthread_mutex_unlock(&_node_mutex);
}
void GZBridge::navSatCallback(const gz::msgs::NavSat &nav_sat)
{
if (hrt_absolute_time() == 0) {
return;
}
pthread_mutex_lock(&_node_mutex);
const uint64_t time_us = (nav_sat.header().stamp().sec() * 1000000) + (nav_sat.header().stamp().nsec() / 1000);
if (time_us > _world_time_us.load()) {
updateClock(nav_sat.header().stamp().sec(), nav_sat.header().stamp().nsec());
}
_timestamp_prev = time_us;
// initialize gps position
if (!_pos_ref.isInitialized()) {
_pos_ref.initReference(nav_sat.latitude_deg(), nav_sat.longitude_deg(), hrt_absolute_time());
_alt_ref = nav_sat.altitude();
} else {
// publish GPS groundtruth
vehicle_global_position_s global_position_groundtruth{};
#if defined(ENABLE_LOCKSTEP_SCHEDULER)
global_position_groundtruth.timestamp_sample = time_us;
#else
global_position_groundtruth.timestamp_sample = hrt_absolute_time();
#endif
global_position_groundtruth.lat = nav_sat.latitude_deg();
global_position_groundtruth.lon = nav_sat.longitude_deg();
global_position_groundtruth.alt = nav_sat.altitude();
_gpos_ground_truth_pub.publish(global_position_groundtruth);
}
pthread_mutex_unlock(&_node_mutex);
}
void GZBridge::rotateQuaternion(gz::math::Quaterniond &q_FRD_to_NED, const gz::math::Quaterniond q_FLU_to_ENU)
{
// FLU (ROS) to FRD (PX4) static rotation
@@ -105,6 +105,7 @@ private:
void imuCallback(const gz::msgs::IMU &imu);
void poseInfoCallback(const gz::msgs::Pose_V &pose);
void odometryCallback(const gz::msgs::OdometryWithCovariance &odometry);
void navSatCallback(const gz::msgs::NavSat &nav_sat);
/**
*
@@ -139,6 +140,7 @@ private:
pthread_mutex_t _node_mutex;
MapProjection _pos_ref{};
double _alt_ref{}; // starting altitude reference
matrix::Vector3d _position_prev{};
matrix::Vector3d _velocity_prev{};
@@ -153,10 +155,4 @@ private:
float _temperature{288.15}; // 15 degrees
gz::transport::Node _node;
DEFINE_PARAMETERS(
(ParamFloat<px4::params::SIM_GZ_HOME_LAT>) _param_sim_home_lat,
(ParamFloat<px4::params::SIM_GZ_HOME_LON>) _param_sim_home_lon,
(ParamFloat<px4::params::SIM_GZ_HOME_ALT>) _param_sim_home_alt
)
};
@@ -40,26 +40,3 @@
*/
PARAM_DEFINE_INT32(SIM_GZ_EN, 0);
/**
* simulator origin latitude
*
* @unit deg
* @group Simulator
*/
PARAM_DEFINE_FLOAT(SIM_GZ_HOME_LAT, 47.397742f);
/**
* simulator origin longitude
*
* @unit deg
* @group Simulator
*/
PARAM_DEFINE_FLOAT(SIM_GZ_HOME_LON, 8.545594);
/**
* simulator origin altitude
*
* @unit m
* @group Simulator
*/
PARAM_DEFINE_FLOAT(SIM_GZ_HOME_ALT, 488.0);
@@ -531,6 +531,140 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
mavlink_hil_state_quaternion_t hil_state;
mavlink_msg_hil_state_quaternion_decode(msg, &hil_state);
if ((hil_state.lat == 0) && (hil_state.lon == 0)) {
_time_us_prev = hil_state.time_usec;
return;
}
float dt_s = (hil_state.time_usec - _time_us_prev) * 1e-6f;
uint64_t timestamp_sample = hrt_absolute_time(); // TODO: HIL_STATE_QUATERNION.time_us
matrix::Quatf q(hil_state.attitude_quaternion);
q.normalize();
const matrix::Eulerf euler(q);
// angular velocity
{
vehicle_angular_velocity_s angular_velocity{};
angular_velocity.timestamp_sample = timestamp_sample;
angular_velocity.xyz[0] = hil_state.rollspeed;
angular_velocity.xyz[1] = hil_state.pitchspeed;
angular_velocity.xyz[2] = hil_state.yawspeed;
angular_velocity.xyz_derivative[0] = (hil_state.rollspeed - _rollspeed_prev) / dt_s;
angular_velocity.xyz_derivative[1] = (hil_state.pitchspeed - _pitchspeed_prev) / dt_s;
angular_velocity.xyz_derivative[2] = (hil_state.yawspeed - _yawspeed_prev) / dt_s;
angular_velocity.timestamp = hrt_absolute_time();
_vehicle_angular_velocity_pub.publish(angular_velocity);
}
// vehicle_acceleration // TODO:
// vehicle_attitude
{
vehicle_attitude_s attitude{};
attitude.timestamp_sample = timestamp_sample;
q.copyTo(attitude.q);
attitude.timestamp = hrt_absolute_time();
_vehicle_attitude_pub.publish(attitude);
}
// vehicle_local_position
{
vehicle_local_position_s local_position{};
local_position.timestamp_sample = timestamp_sample;
double lat = hil_state.lat * 1e-7; // degE7 -> deg
double lon = hil_state.lon * 1e-7; // degE7 -> deg
if (!_global_local_proj_ref.isInitialized() && (hil_state.lon != 0)) {
_global_local_proj_ref.initReference(lat, lon);
_global_local_alt0 = hil_state.alt / 1000.f; // mm -> m
}
if (_global_local_proj_ref.isInitialized()) {
local_position.xy_valid = true;
local_position.z_valid = true;
local_position.v_xy_valid = true;
local_position.v_z_valid = true;
_global_local_proj_ref.project(lat, lon, local_position.x, local_position.y);
local_position.z = _global_local_alt0 - (hil_state.alt / 1000.f); // mm -> m
local_position.vx = hil_state.vx / 100.f; // cm/s -> m/s
local_position.vy = hil_state.vy / 100.f; // cm/s -> m/s
local_position.vz = hil_state.vz / 100.f; // cm/s -> m/s
local_position.z_deriv = local_position.vz;
local_position.ax = hil_state.xacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.ay = hil_state.yacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.az = hil_state.zacc / 1000.f * CONSTANTS_ONE_G; // mG -> m/s/s
local_position.heading = euler.psi();
local_position.unaided_heading = local_position.heading;
local_position.heading_good_for_control = true;
local_position.xy_global = true;
local_position.z_global = true;
local_position.ref_timestamp = _global_local_proj_ref.getProjectionReferenceTimestamp();
local_position.ref_lat = _global_local_proj_ref.getProjectionReferenceLat();
local_position.ref_lon = _global_local_proj_ref.getProjectionReferenceLon();
local_position.ref_alt = _global_local_alt0;
local_position.dist_bottom = NAN;
local_position.eph = 1.f;
local_position.epv = 2.f;
local_position.evh = 1.f;
local_position.evv = 1.f;
local_position.vxy_max = std::numeric_limits<float>::infinity();
local_position.vz_max = std::numeric_limits<float>::infinity();
local_position.hagl_min = std::numeric_limits<float>::infinity();
local_position.hagl_max = std::numeric_limits<float>::infinity();
local_position.timestamp = hrt_absolute_time();
_vehicle_local_position_pub.publish(local_position);
}
}
// global position
{
vehicle_global_position_s global_position{};
global_position.timestamp_sample = timestamp_sample;
global_position.lat = hil_state.lat / 1e7;
global_position.lon = hil_state.lon / 1e7;
global_position.alt = hil_state.alt / 1e3;
global_position.alt_ellipsoid = global_position.alt;
global_position.eph = 1.f;
global_position.epv = 2.f;
global_position.terrain_alt = NAN;
global_position.timestamp = hrt_absolute_time();
_vehicle_global_position_pub.publish(global_position);
}
_time_us_prev = hil_state.time_usec;
_rollspeed_prev = hil_state.rollspeed;
_pitchspeed_prev = hil_state.pitchspeed;
_yawspeed_prev = hil_state.yawspeed;
#if 0
uint64_t timestamp = hrt_absolute_time();
/* angular velocity */
@@ -614,6 +748,8 @@ void SimulatorMavlink::handle_message_hil_state_quaternion(const mavlink_message
// always publish ground truth attitude message
_lpos_ground_truth_pub.publish(hil_lpos);
}
#endif
}
void SimulatorMavlink::handle_message_landing_target(const mavlink_message_t *msg)
@@ -253,6 +253,19 @@ private:
uORB::Publication<vehicle_local_position_s> _lpos_ground_truth_pub{ORB_ID(vehicle_local_position_groundtruth)};
uORB::Publication<input_rc_s> _input_rc_pub{ORB_ID(input_rc)};
uORB::Publication<vehicle_angular_velocity_s> _vehicle_angular_velocity_pub{ORB_ID(vehicle_angular_velocity)};
uORB::Publication<vehicle_attitude_s> _vehicle_attitude_pub{ORB_ID(vehicle_attitude)};
uORB::Publication<vehicle_global_position_s> _vehicle_global_position_pub{ORB_ID(vehicle_global_position)};
uORB::Publication<vehicle_local_position_s> _vehicle_local_position_pub{ORB_ID(vehicle_local_position)};
uORB::Publication<vehicle_odometry_s> _vehicle_odometry_pub{ORB_ID(vehicle_odometry)};
uint64_t _time_us_prev{0};
float _rollspeed_prev{0.f};
float _pitchspeed_prev{0.f};
float _yawspeed_prev{0.f};
//rpm
uORB::Publication<rpm_s> _rpm_pub{ORB_ID(rpm)};
+5
View File
@@ -225,6 +225,10 @@ menu "Zenoh publishers/subscribers"
bool "figure_eight_status"
default n
config ZENOH_PUBSUB_FLIGHT_PHASE_ESTIMATION
bool "flight_phase_estimation"
default n
config ZENOH_PUBSUB_FOLLOW_TARGET
bool "follow_target"
default n
@@ -882,6 +886,7 @@ config ZENOH_PUBSUB_ALL_SELECTION
select ZENOH_PUBSUB_FAILSAFE_FLAGS
select ZENOH_PUBSUB_FAILURE_DETECTOR_STATUS
select ZENOH_PUBSUB_FIGURE_EIGHT_STATUS
select ZENOH_PUBSUB_FLIGHT_PHASE_ESTIMATION
select ZENOH_PUBSUB_FOLLOW_TARGET
select ZENOH_PUBSUB_FOLLOW_TARGET_ESTIMATOR
select ZENOH_PUBSUB_FOLLOW_TARGET_STATUS