mirror of https://github.com/ArduPilot/ardupilot
SITL: document airspeed params
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@ -160,6 +160,11 @@ const AP_Param::GroupInfo SIM::var_info[] = {
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// @Range: 1 10
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// @User: Advanced
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AP_GROUPINFO("SPEEDUP", 52, SIM, speedup, -1),
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// @Param: IMU_POS
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// @DisplayName: IMU Offsets
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// @Description: XYZ position of the IMU accelerometer relative to the body frame origin
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// @Units: m
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// @Vector3Parameter: 1
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AP_GROUPINFO("IMU_POS", 53, SIM, imu_pos_offset, 0),
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AP_SUBGROUPEXTENSION("", 54, SIM, var_ins),
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AP_GROUPINFO("SONAR_POS", 55, SIM, rngfnd_pos_offset, 0),
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@ -353,7 +358,9 @@ const AP_Param::GroupInfo SIM::var_info3[] = {
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AP_GROUPINFO("RATE_HZ", 22, SIM, loop_rate_hz, SIM_RATE_HZ_DEFAULT),
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// count of simulated IMUs
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// @Param: IMU_COUNT
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// @DisplayName: IMU count
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// @Description: Number of simulated IMUs to create
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AP_GROUPINFO("IMU_COUNT", 23, SIM, imu_count, 2),
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// @Path: ./SIM_FETtecOneWireESC.cpp
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@ -432,9 +439,13 @@ const AP_Param::GroupInfo SIM::var_info3[] = {
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// @User: Advanced
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AP_GROUPINFO("UART_LOSS", 42, SIM, uart_byte_loss_pct, 0),
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AP_SUBGROUPINFO(airspeed[0], "ARSPD_", 50, SIM, SIM::AirspeedParm),
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// @Group: ARSPD_
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// @Path: ./SITL_Airspeed.cpp
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AP_SUBGROUPINFO(airspeed[0], "ARSPD_", 50, SIM, AirspeedParm),
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#if AIRSPEED_MAX_SENSORS > 1
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AP_SUBGROUPINFO(airspeed[1], "ARSPD2_", 51, SIM, SIM::AirspeedParm),
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// @Group: ARSPD2_
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// @Path: ./SITL_Airspeed.cpp
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AP_SUBGROUPINFO(airspeed[1], "ARSPD2_", 51, SIM, AirspeedParm),
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#endif
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@ -464,24 +475,6 @@ const AP_Param::GroupInfo SIM::BaroParm::var_info[] = {
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AP_GROUPEND
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};
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// user settable parameters for airspeed sensors
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const AP_Param::GroupInfo SIM::AirspeedParm::var_info[] = {
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// user settable parameters for the 1st airspeed sensor
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AP_GROUPINFO("RND", 1, SIM::AirspeedParm, noise, 2.0),
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AP_GROUPINFO("OFS", 2, SIM::AirspeedParm, offset, 2013),
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// @Param: ARSPD_FAIL
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// @DisplayName: Airspeed sensor failure
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// @Description: Simulates Airspeed sensor 1 failure
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// @Values: 0:Disabled, 1:Enabled
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// @User: Advanced
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AP_GROUPINFO("FAIL", 3, SIM::AirspeedParm, fail, 0),
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AP_GROUPINFO("FAILP", 4, SIM::AirspeedParm, fail_pressure, 0),
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AP_GROUPINFO("PITOT", 5, SIM::AirspeedParm, fail_pitot_pressure, 0),
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AP_GROUPINFO("SIGN", 6, SIM::AirspeedParm, signflip, 0),
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AP_GROUPINFO("RATIO", 7, SIM::AirspeedParm, ratio, 1.99),
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AP_GROUPEND
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};
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#if HAL_SIM_GPS_ENABLED
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// GPS SITL parameters
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const AP_Param::GroupInfo SIM::var_gps[] = {
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@ -0,0 +1,44 @@
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#include "SITL.h"
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#if AP_SIM_ENABLED
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namespace SITL {
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// user settable parameters for airspeed sensors
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const AP_Param::GroupInfo SIM::AirspeedParm::var_info[] = {
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// user settable parameters for the 1st airspeed sensor
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AP_GROUPINFO("RND", 1, AirspeedParm, noise, 2.0),
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AP_GROUPINFO("OFS", 2, AirspeedParm, offset, 2013),
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// @Param: FAIL
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// @DisplayName: Airspeed sensor failure
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// @Description: Simulates Airspeed sensor 1 failure
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// @Values: 0:Disabled, 1:Enabled
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// @User: Advanced
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AP_GROUPINFO("FAIL", 3, AirspeedParm, fail, 0),
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// @Param: FAILP
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// @DisplayName: Airspeed sensor failure pressure
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// @Description: Simulated airspeed sensor failure pressure
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// @Units: Pa
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// @User: Advanced
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AP_GROUPINFO("FAILP", 4, AirspeedParm, fail_pressure, 0),
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// @Param: PITOT
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// @DisplayName: Airspeed pitot tube failure pressure
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// @Description: Simulated airspeed sensor pitot tube failure pressure
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// @Units: Pa
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// @User: Advanced
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AP_GROUPINFO("PITOT", 5, AirspeedParm, fail_pitot_pressure, 0),
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// @Param: SIGN
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// @DisplayName: Airspeed signflip
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// @Description: Simulated airspeed sensor with reversed pitot/static connections
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// @Values: 0:Disabled, 1:Enabled
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// @User: Advanced
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AP_GROUPINFO("SIGN", 6, AirspeedParm, signflip, 0),
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// @Param: RATIO
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// @DisplayName: Airspeed ratios
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// @Description: Simulated airspeed sensor ratio
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// @User: Advanced
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AP_GROUPINFO("RATIO", 7, AirspeedParm, ratio, 1.99),
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AP_GROUPEND
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};
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}
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#endif // AP_SIM_ENABLED
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