mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-20 04:23:33 +08:00
Merge branch 'master' into mpc_local_pos
This commit is contained in:
@@ -0,0 +1,173 @@
|
|||||||
|
# This file is NOT licensed under the GPLv3, which is the license for the rest
|
||||||
|
# of YouCompleteMe.
|
||||||
|
#
|
||||||
|
# Here's the license text for this file:
|
||||||
|
#
|
||||||
|
# This is free and unencumbered software released into the public domain.
|
||||||
|
#
|
||||||
|
# Anyone is free to copy, modify, publish, use, compile, sell, or
|
||||||
|
# distribute this software, either in source code form or as a compiled
|
||||||
|
# binary, for any purpose, commercial or non-commercial, and by any
|
||||||
|
# means.
|
||||||
|
#
|
||||||
|
# In jurisdictions that recognize copyright laws, the author or authors
|
||||||
|
# of this software dedicate any and all copyright interest in the
|
||||||
|
# software to the public domain. We make this dedication for the benefit
|
||||||
|
# of the public at large and to the detriment of our heirs and
|
||||||
|
# successors. We intend this dedication to be an overt act of
|
||||||
|
# relinquishment in perpetuity of all present and future rights to this
|
||||||
|
# software under copyright law.
|
||||||
|
#
|
||||||
|
# THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND,
|
||||||
|
# EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF
|
||||||
|
# MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT.
|
||||||
|
# IN NO EVENT SHALL THE AUTHORS BE LIABLE FOR ANY CLAIM, DAMAGES OR
|
||||||
|
# OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE,
|
||||||
|
# ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR
|
||||||
|
# OTHER DEALINGS IN THE SOFTWARE.
|
||||||
|
#
|
||||||
|
# For more information, please refer to <http://unlicense.org/>
|
||||||
|
|
||||||
|
import os
|
||||||
|
import ycm_core
|
||||||
|
|
||||||
|
# These are the compilation flags that will be used in case there's no
|
||||||
|
# compilation database set (by default, one is not set).
|
||||||
|
# CHANGE THIS LIST OF FLAGS. YES, THIS IS THE DROID YOU HAVE BEEN LOOKING FOR.
|
||||||
|
flags = [
|
||||||
|
'-Wall',
|
||||||
|
'-Wextra',
|
||||||
|
'-Werror',
|
||||||
|
#'-Wc++98-compat',
|
||||||
|
'-Wno-long-long',
|
||||||
|
'-Wno-variadic-macros',
|
||||||
|
'-fexceptions',
|
||||||
|
'-DNDEBUG',
|
||||||
|
# You 100% do NOT need -DUSE_CLANG_COMPLETER in your flags; only the YCM
|
||||||
|
# source code needs it.
|
||||||
|
#'-DUSE_CLANG_COMPLETER',
|
||||||
|
# THIS IS IMPORTANT! Without a "-std=<something>" flag, clang won't know which
|
||||||
|
# language to use when compiling headers. So it will guess. Badly. So C++
|
||||||
|
# headers will be compiled as C headers. You don't want that so ALWAYS specify
|
||||||
|
# a "-std=<something>".
|
||||||
|
# For a C project, you would set this to something like 'c99' instead of
|
||||||
|
# 'c++11'.
|
||||||
|
'-std=c++11',
|
||||||
|
# ...and the same thing goes for the magic -x option which specifies the
|
||||||
|
# language that the files to be compiled are written in. This is mostly
|
||||||
|
# relevant for c++ headers.
|
||||||
|
# For a C project, you would set this to 'c' instead of 'c++'.
|
||||||
|
'-x',
|
||||||
|
'c++',
|
||||||
|
'-undef', # get rid of standard definitions to allow us to include arm math header
|
||||||
|
'-I', os.path.join(os.path.expanduser("~"),'gcc-arm-none-eabi-4_7-2013q3/arm-none-eabi/include'),
|
||||||
|
'-I', 'Build/px4io-v1_default.build/nuttx-export/include/',
|
||||||
|
'-I', 'Build/px4io-v2_default.build/nuttx-export/include/',
|
||||||
|
'-I', './NuttX/nuttx/arch/arm/include',
|
||||||
|
'-include', './src/include/visibility.h',
|
||||||
|
'-I', './src',
|
||||||
|
'-I', './src/modules',
|
||||||
|
'-I', './src/include',
|
||||||
|
'-I', './src/lib',
|
||||||
|
'-I', './NuttX',
|
||||||
|
]
|
||||||
|
|
||||||
|
|
||||||
|
# Set this to the absolute path to the folder (NOT the file!) containing the
|
||||||
|
# compile_commands.json file to use that instead of 'flags'. See here for
|
||||||
|
# more details: http://clang.llvm.org/docs/JSONCompilationDatabase.html
|
||||||
|
#
|
||||||
|
# Most projects will NOT need to set this to anything; you can just change the
|
||||||
|
# 'flags' list of compilation flags. Notice that YCM itself uses that approach.
|
||||||
|
compilation_database_folder = ''
|
||||||
|
|
||||||
|
if os.path.exists( compilation_database_folder ):
|
||||||
|
database = ycm_core.CompilationDatabase( compilation_database_folder )
|
||||||
|
else:
|
||||||
|
database = None
|
||||||
|
|
||||||
|
SOURCE_EXTENSIONS = [ '.cpp', '.cxx', '.cc', '.c', '.m', '.mm' ]
|
||||||
|
|
||||||
|
def DirectoryOfThisScript():
|
||||||
|
return os.path.dirname( os.path.abspath( __file__ ) )
|
||||||
|
|
||||||
|
|
||||||
|
def MakeRelativePathsInFlagsAbsolute( flags, working_directory ):
|
||||||
|
if not working_directory:
|
||||||
|
return list( flags )
|
||||||
|
new_flags = []
|
||||||
|
make_next_absolute = False
|
||||||
|
path_flags = [ '-isystem', '-I', '-iquote', '--sysroot=' ]
|
||||||
|
for flag in flags:
|
||||||
|
new_flag = flag
|
||||||
|
|
||||||
|
if make_next_absolute:
|
||||||
|
make_next_absolute = False
|
||||||
|
if not flag.startswith( '/' ):
|
||||||
|
new_flag = os.path.join( working_directory, flag )
|
||||||
|
|
||||||
|
for path_flag in path_flags:
|
||||||
|
if flag == path_flag:
|
||||||
|
make_next_absolute = True
|
||||||
|
break
|
||||||
|
|
||||||
|
if flag.startswith( path_flag ):
|
||||||
|
path = flag[ len( path_flag ): ]
|
||||||
|
new_flag = path_flag + os.path.join( working_directory, path )
|
||||||
|
break
|
||||||
|
|
||||||
|
if new_flag:
|
||||||
|
new_flags.append( new_flag )
|
||||||
|
return new_flags
|
||||||
|
|
||||||
|
|
||||||
|
def IsHeaderFile( filename ):
|
||||||
|
extension = os.path.splitext( filename )[ 1 ]
|
||||||
|
return extension in [ '.h', '.hxx', '.hpp', '.hh' ]
|
||||||
|
|
||||||
|
|
||||||
|
def GetCompilationInfoForFile( filename ):
|
||||||
|
# The compilation_commands.json file generated by CMake does not have entries
|
||||||
|
# for header files. So we do our best by asking the db for flags for a
|
||||||
|
# corresponding source file, if any. If one exists, the flags for that file
|
||||||
|
# should be good enough.
|
||||||
|
if IsHeaderFile( filename ):
|
||||||
|
basename = os.path.splitext( filename )[ 0 ]
|
||||||
|
for extension in SOURCE_EXTENSIONS:
|
||||||
|
replacement_file = basename + extension
|
||||||
|
if os.path.exists( replacement_file ):
|
||||||
|
compilation_info = database.GetCompilationInfoForFile(
|
||||||
|
replacement_file )
|
||||||
|
if compilation_info.compiler_flags_:
|
||||||
|
return compilation_info
|
||||||
|
return None
|
||||||
|
return database.GetCompilationInfoForFile( filename )
|
||||||
|
|
||||||
|
|
||||||
|
def FlagsForFile( filename, **kwargs ):
|
||||||
|
if database:
|
||||||
|
# Bear in mind that compilation_info.compiler_flags_ does NOT return a
|
||||||
|
# python list, but a "list-like" StringVec object
|
||||||
|
compilation_info = GetCompilationInfoForFile( filename )
|
||||||
|
if not compilation_info:
|
||||||
|
return None
|
||||||
|
|
||||||
|
final_flags = MakeRelativePathsInFlagsAbsolute(
|
||||||
|
compilation_info.compiler_flags_,
|
||||||
|
compilation_info.compiler_working_dir_ )
|
||||||
|
|
||||||
|
# NOTE: This is just for YouCompleteMe; it's highly likely that your project
|
||||||
|
# does NOT need to remove the stdlib flag. DO NOT USE THIS IN YOUR
|
||||||
|
# ycm_extra_conf IF YOU'RE NOT 100% SURE YOU NEED IT.
|
||||||
|
#try:
|
||||||
|
# final_flags.remove( '-stdlib=libc++' )
|
||||||
|
#except ValueError:
|
||||||
|
# pass
|
||||||
|
else:
|
||||||
|
relative_to = DirectoryOfThisScript()
|
||||||
|
final_flags = MakeRelativePathsInFlagsAbsolute( flags, relative_to )
|
||||||
|
|
||||||
|
return {
|
||||||
|
'flags': final_flags,
|
||||||
|
'do_cache': True
|
||||||
|
}
|
||||||
@@ -10,6 +10,7 @@ mavlink start -r 10000 -d /dev/ttyACM0
|
|||||||
mavlink stream -d /dev/ttyACM0 -s NAMED_VALUE_FLOAT -r 10
|
mavlink stream -d /dev/ttyACM0 -s NAMED_VALUE_FLOAT -r 10
|
||||||
mavlink stream -d /dev/ttyACM0 -s OPTICAL_FLOW -r 10
|
mavlink stream -d /dev/ttyACM0 -s OPTICAL_FLOW -r 10
|
||||||
mavlink stream -d /dev/ttyACM0 -s ATTITUDE_CONTROLS -r 30
|
mavlink stream -d /dev/ttyACM0 -s ATTITUDE_CONTROLS -r 30
|
||||||
|
mavlink stream -d /dev/ttyACM0 -s SERVO_OUTPUT_RAW_0 -r 10
|
||||||
|
|
||||||
# Exit shell to make it available to MAVLink
|
# Exit shell to make it available to MAVLink
|
||||||
exit
|
exit
|
||||||
|
|||||||
@@ -79,6 +79,8 @@
|
|||||||
#include <systemlib/param/param.h>
|
#include <systemlib/param/param.h>
|
||||||
#include <systemlib/perf_counter.h>
|
#include <systemlib/perf_counter.h>
|
||||||
|
|
||||||
|
#include <mathlib/math/filter/LowPassFilter2p.hpp>
|
||||||
|
|
||||||
#include <drivers/drv_airspeed.h>
|
#include <drivers/drv_airspeed.h>
|
||||||
#include <drivers/drv_hrt.h>
|
#include <drivers/drv_hrt.h>
|
||||||
|
|
||||||
@@ -99,6 +101,8 @@
|
|||||||
#define ADDR_READ_MR 0x00 /* write to this address to start conversion */
|
#define ADDR_READ_MR 0x00 /* write to this address to start conversion */
|
||||||
|
|
||||||
/* Measurement rate is 100Hz */
|
/* Measurement rate is 100Hz */
|
||||||
|
#define MEAS_RATE 100.0f
|
||||||
|
#define MEAS_DRIVER_FILTER_FREQ 3.0f
|
||||||
#define CONVERSION_INTERVAL (1000000 / 100) /* microseconds */
|
#define CONVERSION_INTERVAL (1000000 / 100) /* microseconds */
|
||||||
|
|
||||||
class MEASAirspeed : public Airspeed
|
class MEASAirspeed : public Airspeed
|
||||||
@@ -116,6 +120,7 @@ protected:
|
|||||||
virtual int measure();
|
virtual int measure();
|
||||||
virtual int collect();
|
virtual int collect();
|
||||||
|
|
||||||
|
math::LowPassFilter2p _filter;
|
||||||
};
|
};
|
||||||
|
|
||||||
/*
|
/*
|
||||||
@@ -124,7 +129,8 @@ protected:
|
|||||||
extern "C" __EXPORT int meas_airspeed_main(int argc, char *argv[]);
|
extern "C" __EXPORT int meas_airspeed_main(int argc, char *argv[]);
|
||||||
|
|
||||||
MEASAirspeed::MEASAirspeed(int bus, int address, const char *path) : Airspeed(bus, address,
|
MEASAirspeed::MEASAirspeed(int bus, int address, const char *path) : Airspeed(bus, address,
|
||||||
CONVERSION_INTERVAL, path)
|
CONVERSION_INTERVAL, path),
|
||||||
|
_filter(MEAS_RATE, MEAS_DRIVER_FILTER_FREQ)
|
||||||
{
|
{
|
||||||
|
|
||||||
}
|
}
|
||||||
@@ -212,6 +218,7 @@ MEASAirspeed::collect()
|
|||||||
report.error_count = perf_event_count(_comms_errors);
|
report.error_count = perf_event_count(_comms_errors);
|
||||||
report.temperature = temperature;
|
report.temperature = temperature;
|
||||||
report.differential_pressure_pa = diff_press_pa;
|
report.differential_pressure_pa = diff_press_pa;
|
||||||
|
report.differential_pressure_filtered_pa = _filter.apply(diff_press_pa);
|
||||||
report.voltage = 0;
|
report.voltage = 0;
|
||||||
report.max_differential_pressure_pa = _max_differential_pressure_pa;
|
report.max_differential_pressure_pa = _max_differential_pressure_pa;
|
||||||
|
|
||||||
|
|||||||
@@ -119,6 +119,7 @@ extern struct system_load_s system_load;
|
|||||||
|
|
||||||
#define POSITION_TIMEOUT 20000 /**< consider the local or global position estimate invalid after 20ms */
|
#define POSITION_TIMEOUT 20000 /**< consider the local or global position estimate invalid after 20ms */
|
||||||
#define RC_TIMEOUT 100000
|
#define RC_TIMEOUT 100000
|
||||||
|
#define RC_TIMEOUT_HIL 500000
|
||||||
#define DIFFPRESS_TIMEOUT 2000000
|
#define DIFFPRESS_TIMEOUT 2000000
|
||||||
|
|
||||||
#define PRINT_INTERVAL 5000000
|
#define PRINT_INTERVAL 5000000
|
||||||
@@ -1099,8 +1100,16 @@ int commander_thread_main(int argc, char *argv[])
|
|||||||
orb_copy(ORB_ID(vehicle_gps_position), gps_sub, &gps_position);
|
orb_copy(ORB_ID(vehicle_gps_position), gps_sub, &gps_position);
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
||||||
|
/*
|
||||||
|
* XXX workaround:
|
||||||
|
* Prevent RC loss in HIL when sensors.cpp is only publishing sp_man at a low rate (e.g. 30Hz)
|
||||||
|
* which can trigger RC loss if the computer/simulator lags.
|
||||||
|
*/
|
||||||
|
uint64_t rc_timeout = status.hil_state == HIL_STATE_ON ? RC_TIMEOUT_HIL : RC_TIMEOUT;
|
||||||
|
|
||||||
/* start RC input check */
|
/* start RC input check */
|
||||||
if (!status.rc_input_blocked && sp_man.timestamp != 0 && hrt_absolute_time() < sp_man.timestamp + RC_TIMEOUT) {
|
if (!status.rc_input_blocked && sp_man.timestamp != 0 && hrt_absolute_time() < sp_man.timestamp + rc_timeout) {
|
||||||
/* handle the case where RC signal was regained */
|
/* handle the case where RC signal was regained */
|
||||||
if (!status.rc_signal_found_once) {
|
if (!status.rc_signal_found_once) {
|
||||||
status.rc_signal_found_once = true;
|
status.rc_signal_found_once = true;
|
||||||
|
|||||||
@@ -71,6 +71,7 @@
|
|||||||
#include <uORB/topics/battery_status.h>
|
#include <uORB/topics/battery_status.h>
|
||||||
#include <uORB/topics/navigation_capabilities.h>
|
#include <uORB/topics/navigation_capabilities.h>
|
||||||
#include <drivers/drv_rc_input.h>
|
#include <drivers/drv_rc_input.h>
|
||||||
|
#include <drivers/drv_pwm_output.h>
|
||||||
|
|
||||||
#include "mavlink_messages.h"
|
#include "mavlink_messages.h"
|
||||||
|
|
||||||
@@ -788,47 +789,79 @@ protected:
|
|||||||
uint32_t mavlink_custom_mode;
|
uint32_t mavlink_custom_mode;
|
||||||
get_mavlink_mode_state(status, pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode);
|
get_mavlink_mode_state(status, pos_sp_triplet, &mavlink_state, &mavlink_base_mode, &mavlink_custom_mode);
|
||||||
|
|
||||||
/* set number of valid outputs depending on vehicle type */
|
if (mavlink_system.type == MAV_TYPE_QUADROTOR ||
|
||||||
unsigned n;
|
mavlink_system.type == MAV_TYPE_HEXAROTOR ||
|
||||||
|
mavlink_system.type == MAV_TYPE_OCTOROTOR) {
|
||||||
|
/* set number of valid outputs depending on vehicle type */
|
||||||
|
unsigned n;
|
||||||
|
|
||||||
switch (mavlink_system.type) {
|
switch (mavlink_system.type) {
|
||||||
case MAV_TYPE_QUADROTOR:
|
case MAV_TYPE_QUADROTOR:
|
||||||
n = 4;
|
n = 4;
|
||||||
break;
|
break;
|
||||||
|
|
||||||
case MAV_TYPE_HEXAROTOR:
|
case MAV_TYPE_HEXAROTOR:
|
||||||
n = 6;
|
n = 6;
|
||||||
break;
|
break;
|
||||||
|
|
||||||
default:
|
default:
|
||||||
n = 8;
|
n = 8;
|
||||||
break;
|
break;
|
||||||
}
|
}
|
||||||
|
|
||||||
/* scale / assign outputs depending on system type */
|
/* scale / assign outputs depending on system type */
|
||||||
float out[8];
|
float out[8];
|
||||||
|
|
||||||
for (unsigned i = 0; i < 8; i++) {
|
for (unsigned i = 0; i < 8; i++) {
|
||||||
if (i < n) {
|
if (i < n) {
|
||||||
if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
|
if (mavlink_base_mode & MAV_MODE_FLAG_SAFETY_ARMED) {
|
||||||
/* scale fake PWM out 900..1200 us to 0..1*/
|
/* scale fake PWM out 900..2100 us to 0..1 for normal multirotors */
|
||||||
out[i] = (act->output[i] - 900.0f) / 1200.0f;
|
out[i] = (act->output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
|
||||||
|
|
||||||
|
} else {
|
||||||
|
/* send 0 when disarmed */
|
||||||
|
out[i] = 0.0f;
|
||||||
|
}
|
||||||
|
|
||||||
} else {
|
} else {
|
||||||
/* send 0 when disarmed */
|
out[i] = -1.0f;
|
||||||
out[i] = 0.0f;
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
mavlink_msg_hil_controls_send(_channel,
|
||||||
|
hrt_absolute_time(),
|
||||||
|
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
|
||||||
|
mavlink_base_mode,
|
||||||
|
0);
|
||||||
|
} else {
|
||||||
|
|
||||||
|
/* fixed wing: scale all channels except throttle -1 .. 1
|
||||||
|
* because we know that we set the mixers up this way
|
||||||
|
*/
|
||||||
|
|
||||||
|
float out[8];
|
||||||
|
|
||||||
|
const float pwm_center = (PWM_HIGHEST_MAX + PWM_LOWEST_MIN) / 2;
|
||||||
|
|
||||||
|
for (unsigned i = 0; i < 8; i++) {
|
||||||
|
if (i != 3) {
|
||||||
|
/* scale fake PWM out 900..2100 us to -1..+1 for normal channels */
|
||||||
|
out[i] = (act->output[i] - pwm_center) / ((PWM_HIGHEST_MAX - PWM_LOWEST_MIN) / 2);
|
||||||
|
|
||||||
|
} else {
|
||||||
|
|
||||||
|
/* scale fake PWM out 900..2100 us to 0..1 for throttle */
|
||||||
|
out[i] = (act->output[i] - PWM_LOWEST_MIN) / (PWM_HIGHEST_MAX - PWM_LOWEST_MIN);
|
||||||
}
|
}
|
||||||
|
|
||||||
} else {
|
|
||||||
out[i] = -1.0f;
|
|
||||||
}
|
}
|
||||||
}
|
|
||||||
|
|
||||||
mavlink_msg_hil_controls_send(_channel,
|
mavlink_msg_hil_controls_send(_channel,
|
||||||
hrt_absolute_time(),
|
hrt_absolute_time(),
|
||||||
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
|
out[0], out[1], out[2], out[3], out[4], out[5], out[6], out[7],
|
||||||
mavlink_base_mode,
|
mavlink_base_mode,
|
||||||
0);
|
0);
|
||||||
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
};
|
};
|
||||||
|
|||||||
@@ -635,13 +635,15 @@ MavlinkReceiver::handle_message_hil_sensor(mavlink_message_t *msg)
|
|||||||
|
|
||||||
hil_battery_status.timestamp = timestamp;
|
hil_battery_status.timestamp = timestamp;
|
||||||
hil_battery_status.voltage_v = 11.1f;
|
hil_battery_status.voltage_v = 11.1f;
|
||||||
|
hil_battery_status.voltage_filtered_v = 11.1f;
|
||||||
hil_battery_status.current_a = 10.0f;
|
hil_battery_status.current_a = 10.0f;
|
||||||
|
hil_battery_status.discharged_mah = -1.0f;
|
||||||
|
|
||||||
if (_battery_pub > 0) {
|
if (_battery_pub > 0) {
|
||||||
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
|
orb_publish(ORB_ID(battery_status), _battery_pub, &hil_battery_status);
|
||||||
|
|
||||||
} else {
|
} else {
|
||||||
_baro_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
|
_battery_pub = orb_advertise(ORB_ID(battery_status), &hil_battery_status);
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|||||||
@@ -1021,6 +1021,7 @@ int sdlog2_thread_main(int argc, char *argv[])
|
|||||||
log_msg.body.log_SENS.baro_alt = buf.sensor.baro_alt_meter;
|
log_msg.body.log_SENS.baro_alt = buf.sensor.baro_alt_meter;
|
||||||
log_msg.body.log_SENS.baro_temp = buf.sensor.baro_temp_celcius;
|
log_msg.body.log_SENS.baro_temp = buf.sensor.baro_temp_celcius;
|
||||||
log_msg.body.log_SENS.diff_pres = buf.sensor.differential_pressure_pa;
|
log_msg.body.log_SENS.diff_pres = buf.sensor.differential_pressure_pa;
|
||||||
|
log_msg.body.log_SENS.diff_pres_filtered = buf.sensor.differential_pressure_filtered_pa;
|
||||||
LOGBUFFER_WRITE_AND_COUNT(SENS);
|
LOGBUFFER_WRITE_AND_COUNT(SENS);
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|||||||
@@ -92,6 +92,7 @@ struct log_SENS_s {
|
|||||||
float baro_alt;
|
float baro_alt;
|
||||||
float baro_temp;
|
float baro_temp;
|
||||||
float diff_pres;
|
float diff_pres;
|
||||||
|
float diff_pres_filtered;
|
||||||
};
|
};
|
||||||
|
|
||||||
/* --- LPOS - LOCAL POSITION --- */
|
/* --- LPOS - LOCAL POSITION --- */
|
||||||
@@ -306,7 +307,7 @@ static const struct log_format_s log_formats[] = {
|
|||||||
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
|
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
|
||||||
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
|
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
|
||||||
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
|
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
|
||||||
LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres"),
|
LOG_FORMAT(SENS, "fffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"),
|
||||||
LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"),
|
LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"),
|
||||||
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
|
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
|
||||||
LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
|
LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
|
||||||
|
|||||||
@@ -1029,10 +1029,11 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
|
|||||||
|
|
||||||
raw.differential_pressure_pa = _diff_pres.differential_pressure_pa;
|
raw.differential_pressure_pa = _diff_pres.differential_pressure_pa;
|
||||||
raw.differential_pressure_timestamp = _diff_pres.timestamp;
|
raw.differential_pressure_timestamp = _diff_pres.timestamp;
|
||||||
|
raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa;
|
||||||
|
|
||||||
_airspeed.timestamp = hrt_absolute_time();
|
_airspeed.timestamp = _diff_pres.timestamp;
|
||||||
_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_pa);
|
_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_filtered_pa);
|
||||||
_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_pa + raw.baro_pres_mbar * 1e2f,
|
_airspeed.true_airspeed_m_s = calc_true_airspeed(_diff_pres.differential_pressure_filtered_pa + raw.baro_pres_mbar * 1e2f,
|
||||||
raw.baro_pres_mbar * 1e2f, raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
|
raw.baro_pres_mbar * 1e2f, raw.baro_temp_celcius - PCB_TEMP_ESTIMATE_DEG);
|
||||||
|
|
||||||
/* announce the airspeed if needed, just publish else */
|
/* announce the airspeed if needed, just publish else */
|
||||||
|
|||||||
@@ -54,8 +54,9 @@
|
|||||||
struct differential_pressure_s {
|
struct differential_pressure_s {
|
||||||
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
|
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
|
||||||
uint64_t error_count;
|
uint64_t error_count;
|
||||||
float differential_pressure_pa; /**< Differential pressure reading */
|
float differential_pressure_pa; /**< Differential pressure reading */
|
||||||
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
|
float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
|
||||||
|
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
|
||||||
float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
|
float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
|
||||||
float temperature; /**< Temperature provided by sensor */
|
float temperature; /**< Temperature provided by sensor */
|
||||||
|
|
||||||
|
|||||||
@@ -104,6 +104,8 @@ struct sensor_combined_s {
|
|||||||
|
|
||||||
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
|
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
|
||||||
uint64_t differential_pressure_timestamp; /**< Last measurement timestamp */
|
uint64_t differential_pressure_timestamp; /**< Last measurement timestamp */
|
||||||
|
float differential_pressure_filtered_pa; /**< Low pass filtered airspeed sensor differential pressure reading */
|
||||||
|
|
||||||
};
|
};
|
||||||
|
|
||||||
/**
|
/**
|
||||||
|
|||||||
Reference in New Issue
Block a user