mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
This reverts commit 7e45f4915208b2d02e05e5741ff7456cf92120f9. Co-authored-by: jmackay2 <1.732mackay@gmail.com>
This commit is contained in:
parent
0931179579
commit
f252e20eae
@ -33,7 +33,7 @@ param set-default PWM_MAIN_FUNC3 103
|
||||
param set-default PWM_MAIN_FUNC4 104
|
||||
param set-default PWM_MAIN_FUNC5 0
|
||||
|
||||
param set-default FD_FAIL_R 70
|
||||
parm set-default FD_FAIL_R 70
|
||||
|
||||
param set-default FW_P_TC 0.6
|
||||
|
||||
|
||||
@ -14,7 +14,9 @@ PX4_SIM_MODEL=${PX4_SIM_MODEL:=standard_vtol}
|
||||
param set-default SIM_GZ_EN 1
|
||||
|
||||
param set-default SENS_EN_GPSSIM 1
|
||||
param set-default SENS_EN_BAROSIM 0
|
||||
param set-default SENS_EN_MAGSIM 1
|
||||
param set-default SENS_EN_ARSPDSIM 1
|
||||
|
||||
# TODO: Enable motor failure detection when the
|
||||
# VTOL no longer reports 0A for all ESCs in SITL
|
||||
|
||||
@ -1,92 +0,0 @@
|
||||
#!/bin/sh
|
||||
#
|
||||
# @name Quadrotor + Tailsitter
|
||||
#
|
||||
# @type VTOL Quad Tailsitter
|
||||
#
|
||||
|
||||
. ${R}etc/init.d/rc.vtol_defaults
|
||||
|
||||
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
|
||||
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
|
||||
PX4_SIM_MODEL=${PX4_SIM_MODEL:=quadtailsitter}
|
||||
|
||||
param set-default SIM_GZ_EN 1
|
||||
|
||||
param set-default SENS_EN_GPSSIM 1
|
||||
param set-default SENS_EN_BAROSIM 0
|
||||
param set-default SENS_EN_MAGSIM 1
|
||||
param set-default SENS_EN_ARSPDSIM 0
|
||||
|
||||
param set-default MAV_TYPE 20
|
||||
|
||||
param set-default CA_AIRFRAME 4
|
||||
|
||||
param set-default CA_ROTOR_COUNT 4
|
||||
param set-default CA_ROTOR0_PX 0.15
|
||||
param set-default CA_ROTOR0_PY 0.23
|
||||
param set-default CA_ROTOR0_KM 0.05
|
||||
param set-default CA_ROTOR1_PX -0.15
|
||||
param set-default CA_ROTOR1_PY -0.23
|
||||
param set-default CA_ROTOR1_KM 0.05
|
||||
param set-default CA_ROTOR2_PX 0.15
|
||||
param set-default CA_ROTOR2_PY -0.23
|
||||
param set-default CA_ROTOR2_KM -0.05
|
||||
param set-default CA_ROTOR3_PX -0.15
|
||||
param set-default CA_ROTOR3_PY 0.23
|
||||
param set-default CA_ROTOR3_KM -0.05
|
||||
|
||||
param set-default CA_SV_CS_COUNT 0
|
||||
|
||||
param set-default SIM_GZ_EC_FUNC1 101
|
||||
param set-default SIM_GZ_EC_MIN1 10
|
||||
param set-default SIM_GZ_EC_MAX1 1500
|
||||
param set-default SIM_GZ_EC_FUNC2 102
|
||||
param set-default SIM_GZ_EC_MIN2 10
|
||||
param set-default SIM_GZ_EC_MAX2 1500
|
||||
param set-default SIM_GZ_EC_FUNC3 103
|
||||
param set-default SIM_GZ_EC_MIN3 10
|
||||
param set-default SIM_GZ_EC_MAX3 1500
|
||||
param set-default SIM_GZ_EC_FUNC4 104
|
||||
param set-default SIM_GZ_EC_MIN4 10
|
||||
param set-default SIM_GZ_EC_MAX4 1500
|
||||
|
||||
param set-default FD_FAIL_R 70
|
||||
|
||||
param set-default FW_P_TC 0.6
|
||||
|
||||
param set-default FW_PR_I 0.3
|
||||
param set-default FW_PR_P 0.5
|
||||
param set-default FW_PSP_OFF 2
|
||||
param set-default FW_RR_FF 0.1
|
||||
param set-default FW_RR_I 0.1
|
||||
param set-default FW_RR_P 0.2
|
||||
param set-default FW_YR_FF 0 # make yaw rate controller very weak, only keep default P
|
||||
param set-default FW_YR_I 0
|
||||
param set-default FW_THR_TRIM 0.35
|
||||
param set-default FW_THR_MAX 0.8
|
||||
param set-default FW_THR_MIN 0.05
|
||||
param set-default FW_T_CLMB_MAX 6
|
||||
param set-default FW_T_HRATE_FF 0.5
|
||||
param set-default FW_T_SINK_MAX 3
|
||||
param set-default FW_T_SINK_MIN 1.6
|
||||
param set-default FW_AIRSPD_STALL 10
|
||||
param set-default FW_AIRSPD_MIN 14
|
||||
param set-default FW_AIRSPD_TRIM 18
|
||||
param set-default FW_AIRSPD_MAX 22
|
||||
|
||||
param set-default MC_AIRMODE 2
|
||||
param set-default MAN_ARM_GESTURE 0 # required for yaw airmode
|
||||
param set-default MC_ROLL_P 3
|
||||
param set-default MC_PITCH_P 3
|
||||
param set-default MC_ROLLRATE_P 0.3
|
||||
param set-default MC_PITCHRATE_P 0.3
|
||||
|
||||
param set-default VT_ARSP_TRANS 15
|
||||
param set-default VT_B_TRANS_DUR 5
|
||||
param set-default VT_FW_DIFTHR_EN 7
|
||||
param set-default VT_FW_DIFTHR_S_Y 1
|
||||
param set-default VT_F_TRANS_DUR 1.5
|
||||
param set-default VT_TYPE 0
|
||||
|
||||
param set-default WV_EN 0
|
||||
@ -85,7 +85,6 @@ px4_add_romfs_files(
|
||||
4011_gz_lawnmower
|
||||
4012_gz_rover_ackermann
|
||||
4013_gz_x500_lidar
|
||||
4014_gz_quadtailsitter
|
||||
|
||||
6011_gazebo-classic_typhoon_h480
|
||||
6011_gazebo-classic_typhoon_h480.post
|
||||
|
||||
@ -203,15 +203,17 @@ int GZBridge::init()
|
||||
PX4_WARN("failed to subscribe to %s", laser_scan_topic.c_str());
|
||||
}
|
||||
|
||||
// Airspeed: /world/$WORLD/model/$MODEL/link/base_link/sensor/airspeed_sensor/air_speed
|
||||
std::string airspeed_topic = "/world/" + _world_name + "/model/" + _model_name +
|
||||
"/link/base_link/sensor/airspeed_sensor/air_speed";
|
||||
#if 0
|
||||
// Airspeed: /world/$WORLD/model/$MODEL/link/airspeed_link/sensor/air_speed/air_speed
|
||||
std::string airpressure_topic = "/world/" + _world_name + "/model/" + _model_name +
|
||||
"/link/airspeed_link/sensor/air_speed/air_speed";
|
||||
|
||||
if (!_node.Subscribe(airspeed_topic, &GZBridge::airspeedCallback, this)) {
|
||||
PX4_ERR("failed to subscribe to %s", airspeed_topic.c_str());
|
||||
if (!_node.Subscribe(airpressure_topic, &GZBridge::airspeedCallback, this)) {
|
||||
PX4_ERR("failed to subscribe to %s", airpressure_topic.c_str());
|
||||
return PX4_ERROR;
|
||||
}
|
||||
|
||||
#endif
|
||||
// Air pressure: /world/$WORLD/model/$MODEL/link/base_link/sensor/air_pressure_sensor/air_pressure
|
||||
std::string air_pressure_topic = "/world/" + _world_name + "/model/" + _model_name +
|
||||
"/link/base_link/sensor/air_pressure_sensor/air_pressure";
|
||||
@ -424,7 +426,8 @@ void GZBridge::barometerCallback(const gz::msgs::FluidPressure &air_pressure)
|
||||
pthread_mutex_unlock(&_node_mutex);
|
||||
}
|
||||
|
||||
void GZBridge::airspeedCallback(const gz::msgs::AirSpeed &air_speed)
|
||||
#if 0
|
||||
void GZBridge::airspeedCallback(const gz::msgs::AirSpeedSensor &air_speed)
|
||||
{
|
||||
if (hrt_absolute_time() == 0) {
|
||||
return;
|
||||
@ -449,6 +452,7 @@ void GZBridge::airspeedCallback(const gz::msgs::AirSpeed &air_speed)
|
||||
|
||||
pthread_mutex_unlock(&_node_mutex);
|
||||
}
|
||||
#endif
|
||||
|
||||
void GZBridge::imuCallback(const gz::msgs::IMU &imu)
|
||||
{
|
||||
|
||||
@ -102,7 +102,7 @@ private:
|
||||
|
||||
void clockCallback(const gz::msgs::Clock &clock);
|
||||
|
||||
void airspeedCallback(const gz::msgs::AirSpeed &air_speed);
|
||||
// void airspeedCallback(const gz::msgs::AirSpeedSensor &air_pressure);
|
||||
void barometerCallback(const gz::msgs::FluidPressure &air_pressure);
|
||||
void imuCallback(const gz::msgs::IMU &imu);
|
||||
void poseInfoCallback(const gz::msgs::Pose_V &pose);
|
||||
@ -123,7 +123,7 @@ private:
|
||||
// Subscriptions
|
||||
uORB::SubscriptionInterval _parameter_update_sub{ORB_ID(parameter_update), 1_s};
|
||||
|
||||
uORB::Publication<differential_pressure_s> _differential_pressure_pub{ORB_ID(differential_pressure)};
|
||||
//uORB::Publication<differential_pressure_s> _differential_pressure_pub{ORB_ID(differential_pressure)};
|
||||
uORB::Publication<obstacle_distance_s> _obstacle_distance_pub{ORB_ID(obstacle_distance)};
|
||||
uORB::Publication<vehicle_angular_velocity_s> _angular_velocity_ground_truth_pub{ORB_ID(vehicle_angular_velocity_groundtruth)};
|
||||
uORB::Publication<vehicle_attitude_s> _attitude_ground_truth_pub{ORB_ID(vehicle_attitude_groundtruth)};
|
||||
|
||||
@ -195,7 +195,7 @@ int SensorAirspeedSim::print_usage(const char *reason)
|
||||
|
||||
)DESCR_STR");
|
||||
|
||||
PRINT_MODULE_USAGE_NAME("sensor_airspeed_sim", "system");
|
||||
PRINT_MODULE_USAGE_NAME("sensor_arispeed_sim", "system");
|
||||
PRINT_MODULE_USAGE_COMMAND("start");
|
||||
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
|
||||
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user