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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-18 00:03:33 +08:00
Merged master into vision_estimate
This commit is contained in:
@@ -40,6 +40,7 @@
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#include "topics/parameter_update.h"
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#include "topics/actuator_controls.h"
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#include "topics/vehicle_gps_position.h"
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#include "topics/satellite_info.h"
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#include "topics/sensor_combined.h"
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#include "topics/vehicle_attitude.h"
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#include "topics/vehicle_global_position.h"
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@@ -88,6 +89,7 @@ T Subscription<T>::getData() {
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template class __EXPORT Subscription<parameter_update_s>;
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template class __EXPORT Subscription<actuator_controls_s>;
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template class __EXPORT Subscription<vehicle_gps_position_s>;
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template class __EXPORT Subscription<satellite_info_s>;
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template class __EXPORT Subscription<sensor_combined_s>;
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template class __EXPORT Subscription<vehicle_attitude_s>;
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template class __EXPORT Subscription<vehicle_global_position_s>;
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@@ -75,6 +75,9 @@ ORB_DEFINE(sensor_combined, struct sensor_combined_s);
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#include "topics/vehicle_gps_position.h"
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ORB_DEFINE(vehicle_gps_position, struct vehicle_gps_position_s);
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#include "topics/satellite_info.h"
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ORB_DEFINE(satellite_info, struct satellite_info_s);
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#include "topics/home_position.h"
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ORB_DEFINE(home_position, struct home_position_s);
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@@ -183,7 +186,10 @@ ORB_DEFINE(actuator_outputs_2, struct actuator_outputs_s);
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ORB_DEFINE(actuator_outputs_3, struct actuator_outputs_s);
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#include "topics/telemetry_status.h"
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ORB_DEFINE(telemetry_status, struct telemetry_status_s);
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ORB_DEFINE(telemetry_status_0, struct telemetry_status_s);
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ORB_DEFINE(telemetry_status_1, struct telemetry_status_s);
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ORB_DEFINE(telemetry_status_2, struct telemetry_status_s);
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ORB_DEFINE(telemetry_status_3, struct telemetry_status_s);
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#include "topics/debug_key_value.h"
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ORB_DEFINE(debug_key_value, struct debug_key_value_s);
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@@ -203,6 +209,9 @@ ORB_DEFINE(estimator_status, struct estimator_status_report);
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#include "topics/vision_position_estimate.h"
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ORB_DEFINE(vision_position_estimate, struct vision_position_estimate);
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#include "topics/vehicle_force_setpoint.h"
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ORB_DEFINE(vehicle_force_setpoint, struct vehicle_force_setpoint_s);
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#include "topics/tecs_status.h"
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ORB_DEFINE(tecs_status, struct tecs_status_s);
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@@ -98,6 +98,7 @@ struct manual_control_setpoint_s {
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switch_pos_t posctl_switch; /**< position control 2 position switch (optional): _ALTCTL_, POSCTL */
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switch_pos_t loiter_switch; /**< loiter 2 position switch (optional): _MISSION_, LOITER */
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switch_pos_t acro_switch; /**< acro 2 position switch (optional): _MANUAL_, ACRO */
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switch_pos_t offboard_switch; /**< offboard 2 position switch (optional): _NORMAL_, OFFBOARD */
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}; /**< manual control inputs */
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/**
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@@ -69,7 +69,7 @@ struct offboard_control_setpoint_s {
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uint64_t timestamp;
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enum OFFBOARD_CONTROL_MODE mode; /**< The current control inputs mode */
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bool armed; /**< Armed flag set, yes / no */
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float p1; /**< ailerons roll / roll rate input */
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float p2; /**< elevator / pitch / pitch rate */
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float p3; /**< rudder / yaw rate / yaw */
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@@ -60,16 +60,26 @@ enum SETPOINT_TYPE
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SETPOINT_TYPE_TAKEOFF, /**< takeoff setpoint */
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SETPOINT_TYPE_LAND, /**< land setpoint, altitude must be ignored, descend until landing */
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SETPOINT_TYPE_IDLE, /**< do nothing, switch off motors or keep at idle speed (MC) */
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SETPOINT_TYPE_OFFBOARD, /**< setpoint set by offboard */
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};
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struct position_setpoint_s
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{
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bool valid; /**< true if setpoint is valid */
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enum SETPOINT_TYPE type; /**< setpoint type to adjust behavior of position controller */
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float x; /**< local position setpoint in m in NED */
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float y; /**< local position setpoint in m in NED */
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float z; /**< local position setpoint in m in NED */
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bool position_valid; /**< true if local position setpoint valid */
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float vx; /**< local velocity setpoint in m in NED */
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float vy; /**< local velocity setpoint in m in NED */
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float vz; /**< local velocity setpoint in m in NED */
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bool velocity_valid; /**< true if local velocity setpoint valid */
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double lat; /**< latitude, in deg */
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double lon; /**< longitude, in deg */
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float alt; /**< altitude AMSL, in m */
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float yaw; /**< yaw (only for multirotors), in rad [-PI..PI), NaN = hold current yaw */
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float yawspeed; /**< yawspeed (only for multirotors, in rad/s) */
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float loiter_radius; /**< loiter radius (only for fixed wing), in m */
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int8_t loiter_direction; /**< loiter direction: 1 = CW, -1 = CCW */
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float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
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@@ -56,7 +56,7 @@ enum RC_CHANNELS_FUNCTION {
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RETURN,
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POSCTL,
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LOITER,
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OFFBOARD_MODE,
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OFFBOARD,
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ACRO,
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FLAPS,
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AUX_1,
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@@ -0,0 +1,89 @@
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/****************************************************************************
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*
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* Copyright (C) 2014 PX4 Development Team. All rights reserved.
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* Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
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* @author Julian Oes <joes@student.ethz.ch>
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* @author Lorenz Meier <lm@inf.ethz.ch>
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file satellite_info.h
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* Definition of the GNSS satellite info uORB topic.
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*/
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#ifndef TOPIC_SAT_INFO_H_
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#define TOPIC_SAT_INFO_H_
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#include <stdint.h>
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#include "../uORB.h"
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/**
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* @addtogroup topics
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* @{
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*/
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/**
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* GNSS Satellite Info.
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*/
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#define SAT_INFO_MAX_SATELLITES 20
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struct satellite_info_s {
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uint64_t timestamp; /**< Timestamp of satellite info */
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uint8_t count; /**< Number of satellites in satellite info */
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uint8_t svid[SAT_INFO_MAX_SATELLITES]; /**< Space vehicle ID [1..255], see scheme below */
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uint8_t used[SAT_INFO_MAX_SATELLITES]; /**< 0: Satellite not used, 1: used for navigation */
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uint8_t elevation[SAT_INFO_MAX_SATELLITES]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
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uint8_t azimuth[SAT_INFO_MAX_SATELLITES]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
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uint8_t snr[SAT_INFO_MAX_SATELLITES]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
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};
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/**
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* NAV_SVINFO space vehicle ID (svid) scheme according to u-blox protocol specs
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* u-bloxM8-V15_ReceiverDescriptionProtocolSpec_Public_(UBX-13003221).pdf
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*
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* GPS 1-32
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* SBAS 120-158
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* Galileo 211-246
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* BeiDou 159-163, 33-64
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* QZSS 193-197
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* GLONASS 65-96, 255
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*
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*/
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/**
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* @}
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*/
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/* register this as object request broker structure */
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ORB_DECLARE(satellite_info);
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#endif
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@@ -72,6 +72,28 @@ struct telemetry_status_s {
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* @}
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*/
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ORB_DECLARE(telemetry_status);
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ORB_DECLARE(telemetry_status_0);
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ORB_DECLARE(telemetry_status_1);
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ORB_DECLARE(telemetry_status_2);
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ORB_DECLARE(telemetry_status_3);
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#define TELEMETRY_STATUS_ORB_ID_NUM 4
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static const struct orb_metadata *telemetry_status_orb_id[TELEMETRY_STATUS_ORB_ID_NUM] = {
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ORB_ID(telemetry_status_0),
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ORB_ID(telemetry_status_1),
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ORB_ID(telemetry_status_2),
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ORB_ID(telemetry_status_3),
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};
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// This is a hack to quiet an unused-variable warning for when telemetry_status.h is
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// included but telemetry_status_orb_id is not referenced. The inline works if you
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// choose to use it, but you can continue to just directly index into the array as well.
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// If you don't use the inline this ends up being a no-op with no additional code emitted.
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extern inline const struct orb_metadata *telemetry_status_orb_id_lookup(size_t index);
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extern inline const struct orb_metadata *telemetry_status_orb_id_lookup(size_t index)
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{
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return telemetry_status_orb_id[index];
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}
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#endif /* TOPIC_TELEMETRY_STATUS_H */
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@@ -74,6 +74,7 @@ struct vehicle_control_mode_s {
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bool flag_control_manual_enabled; /**< true if manual input is mixed in */
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bool flag_control_auto_enabled; /**< true if onboard autopilot should act */
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bool flag_control_offboard_enabled; /**< true if offboard control should be used */
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bool flag_control_rates_enabled; /**< true if rates are stabilized */
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bool flag_control_attitude_enabled; /**< true if attitude stabilization is mixed in */
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bool flag_control_velocity_enabled; /**< true if horizontal velocity (implies direction) is controlled */
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@@ -0,0 +1,65 @@
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/****************************************************************************
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*
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* Copyright (C) 2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file vehicle_force_setpoint.h
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* @author Thomas Gubler <thomasgubler@gmail.com>
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* Definition of force (NED) setpoint uORB topic. Typically this can be used
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* by a position control app together with an attitude control app.
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*/
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#ifndef TOPIC_VEHICLE_FORCE_SETPOINT_H_
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#define TOPIC_VEHICLE_FORCE_SETPOINT_H_
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#include "../uORB.h"
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/**
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* @addtogroup topics
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* @{
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*/
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struct vehicle_force_setpoint_s {
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float x; /**< in N NED */
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float y; /**< in N NED */
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float z; /**< in N NED */
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float yaw; /**< right-hand rotation around downward axis (rad, equivalent to Tait-Bryan yaw) */
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}; /**< Desired force in NED frame */
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/**
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* @}
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*/
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/* register this as object request broker structure */
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ORB_DECLARE(vehicle_force_setpoint);
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#endif
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@@ -61,7 +61,6 @@ struct vehicle_gps_position_s {
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uint64_t timestamp_variance;
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float s_variance_m_s; /**< speed accuracy estimate m/s */
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float p_variance_m; /**< position accuracy estimate m */
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float c_variance_rad; /**< course accuracy estimate rad */
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uint8_t fix_type; /**< 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. */
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@@ -82,14 +81,7 @@ struct vehicle_gps_position_s {
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uint64_t timestamp_time; /**< Timestamp for time information */
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uint64_t time_gps_usec; /**< Timestamp (microseconds in GPS format), this is the timestamp which comes from the gps module */
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uint64_t timestamp_satellites; /**< Timestamp for sattelite information */
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uint8_t satellites_visible; /**< Number of satellites visible. If unknown, set to 255 */
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uint8_t satellite_prn[20]; /**< Global satellite ID */
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uint8_t satellite_used[20]; /**< 0: Satellite not used, 1: used for localization */
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uint8_t satellite_elevation[20]; /**< Elevation (0: right on top of receiver, 90: on the horizon) of satellite */
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uint8_t satellite_azimuth[20]; /**< Direction of satellite, 0: 0 deg, 255: 360 deg. */
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uint8_t satellite_snr[20]; /**< dBHz, Signal to noise ratio of satellite C/N0, range 0..99, zero when not tracking this satellite. */
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bool satellite_info_available; /**< 0 for no info, 1 for info available */
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uint8_t satellites_used; /**< Number of satellites used */
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};
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/**
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@@ -70,7 +70,8 @@ typedef enum {
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MAIN_STATE_AUTO_LOITER,
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MAIN_STATE_AUTO_RTL,
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MAIN_STATE_ACRO,
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MAIN_STATE_MAX,
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MAIN_STATE_OFFBOARD,
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MAIN_STATE_MAX
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} main_state_t;
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// If you change the order, add or remove arming_state_t states make sure to update the arrays
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@@ -106,6 +107,7 @@ typedef enum {
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NAVIGATION_STATE_LAND, /**< Land mode */
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NAVIGATION_STATE_DESCEND, /**< Descend mode (no position control) */
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NAVIGATION_STATE_TERMINATION, /**< Termination mode */
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NAVIGATION_STATE_OFFBOARD,
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NAVIGATION_STATE_MAX,
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} navigation_state_t;
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