mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-27 04:00:05 +08:00
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5 Commits
| Author | SHA1 | Date | |
|---|---|---|---|
| 50cac20187 | |||
| 0770e740b5 | |||
| afa4a22424 | |||
| 068d43e5cd | |||
| ee03c8c3b9 |
@@ -55,7 +55,6 @@ param set-default RWTO_TKOFF 1
|
||||
param set-default CA_AIRFRAME 1
|
||||
|
||||
param set-default COM_PREARM_MODE 2
|
||||
param set-default CBRK_AIRSPD_CHK 162128
|
||||
|
||||
param set-default CA_ROTOR_COUNT 1
|
||||
param set-default CA_ROTOR0_PX 0.3
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||||
|
||||
@@ -0,0 +1,104 @@
|
||||
#!/bin/sh
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||||
#
|
||||
# @name Standard VTOL
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||||
#
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||||
# @type Standard VTOL
|
||||
#
|
||||
|
||||
. ${R}etc/init.d/rc.vtol_defaults
|
||||
|
||||
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
|
||||
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
|
||||
PX4_SIM_MODEL=${PX4_SIM_MODEL:=standard_vtol}
|
||||
|
||||
# TODO: Enable motor failure detection when the
|
||||
# VTOL no longer reports 0A for all ESCs in SITL
|
||||
param set-default FD_ACT_EN 0
|
||||
param set-default FD_ACT_MOT_TOUT 500
|
||||
|
||||
param set-default CA_AIRFRAME 2
|
||||
|
||||
param set-default COM_PREARM_MODE 2
|
||||
|
||||
param set-default CA_ROTOR_COUNT 5
|
||||
param set-default CA_ROTOR0_PX 0.1515
|
||||
param set-default CA_ROTOR0_PY 0.245
|
||||
param set-default CA_ROTOR0_KM 0.05
|
||||
param set-default CA_ROTOR1_PX -0.1515
|
||||
param set-default CA_ROTOR1_PY -0.1875
|
||||
param set-default CA_ROTOR1_KM 0.05
|
||||
param set-default CA_ROTOR2_PX 0.1515
|
||||
param set-default CA_ROTOR2_PY -0.245
|
||||
param set-default CA_ROTOR2_KM -0.05
|
||||
param set-default CA_ROTOR3_PX -0.1515
|
||||
param set-default CA_ROTOR3_PY 0.1875
|
||||
param set-default CA_ROTOR3_KM -0.05
|
||||
param set-default CA_ROTOR4_AX 1.0
|
||||
param set-default CA_ROTOR4_AZ 0.0
|
||||
param set-default CA_ROTOR4_PX 0.2
|
||||
|
||||
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 SIM_GZ_EC_FUNC5 105
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||||
param set-default SIM_GZ_EC_MIN5 0
|
||||
param set-default SIM_GZ_EC_MAX5 3500
|
||||
|
||||
param set-default SIM_GZ_SV_FUNC1 201
|
||||
param set-default SIM_GZ_SV_FUNC2 202
|
||||
param set-default SIM_GZ_SV_FUNC3 203
|
||||
|
||||
param set-default COM_RC_IN_MODE 1
|
||||
param set-default ASPD_PRIMARY 1
|
||||
|
||||
param set-default CA_SV_CS_COUNT 3
|
||||
param set-default CA_SV_CS0_TYPE 1
|
||||
param set-default CA_SV_CS0_TRQ_R -0.5
|
||||
param set-default CA_SV_CS1_TYPE 2
|
||||
param set-default CA_SV_CS1_TRQ_R 0.5
|
||||
param set-default CA_SV_CS2_TYPE 3
|
||||
param set-default CA_SV_CS2_TRQ_P 1.0
|
||||
|
||||
param set-default FW_L1_PERIOD 12
|
||||
param set-default FW_PR_FF 0.2
|
||||
param set-default FW_PR_P 0.9
|
||||
param set-default FW_PSP_OFF 2
|
||||
param set-default FW_P_LIM_MIN -15
|
||||
param set-default FW_RR_FF 0.1
|
||||
param set-default FW_RR_P 0.3
|
||||
param set-default FW_THR_TRIM 0.25
|
||||
param set-default FW_THR_MAX 0.6
|
||||
param set-default FW_THR_MIN 0.05
|
||||
param set-default FW_T_CLMB_MAX 8
|
||||
param set-default FW_T_SINK_MAX 2.7
|
||||
param set-default FW_T_SINK_MIN 2.2
|
||||
|
||||
param set-default MC_AIRMODE 1
|
||||
param set-default MC_ROLLRATE_P 0.3
|
||||
param set-default MC_YAW_P 1.6
|
||||
|
||||
param set-default MIS_TAKEOFF_ALT 10
|
||||
|
||||
param set-default MPC_ACC_HOR_MAX 2
|
||||
param set-default MPC_XY_P 0.8
|
||||
param set-default MPC_XY_VEL_P_ACC 3
|
||||
param set-default MPC_XY_VEL_I_ACC 4
|
||||
param set-default MPC_XY_VEL_D_ACC 0.1
|
||||
|
||||
param set-default NAV_ACC_RAD 5
|
||||
|
||||
param set-default VT_FWD_THRUST_EN 4
|
||||
param set-default VT_F_TRANS_THR 0.75
|
||||
param set-default VT_B_TRANS_DUR 8
|
||||
param set-default VT_TYPE 2
|
||||
param set-default FD_ESCS_EN 0
|
||||
@@ -0,0 +1,102 @@
|
||||
#!/bin/sh
|
||||
#
|
||||
# @name Foxtech Loong
|
||||
#
|
||||
# @type Standard VTOL
|
||||
#
|
||||
|
||||
. ${R}etc/init.d/rc.vtol_defaults
|
||||
|
||||
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
|
||||
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
|
||||
PX4_SIM_MODEL=${PX4_SIM_MODEL:=foxtech_loong_2160}
|
||||
|
||||
# TODO: Enable motor failure detection when the
|
||||
# VTOL no longer reports 0A for all ESCs in SITL
|
||||
param set-default FD_ACT_EN 0
|
||||
param set-default FD_ACT_MOT_TOUT 500
|
||||
|
||||
param set-default CA_AIRFRAME 2
|
||||
|
||||
param set-default CA_ROTOR_COUNT 5
|
||||
param set-default CA_ROTOR0_PX 0.1515
|
||||
param set-default CA_ROTOR0_PY 0.245
|
||||
param set-default CA_ROTOR0_KM 0.05
|
||||
param set-default CA_ROTOR1_PX -0.1515
|
||||
param set-default CA_ROTOR1_PY -0.1875
|
||||
param set-default CA_ROTOR1_KM 0.05
|
||||
param set-default CA_ROTOR2_PX 0.1515
|
||||
param set-default CA_ROTOR2_PY -0.245
|
||||
param set-default CA_ROTOR2_KM -0.05
|
||||
param set-default CA_ROTOR3_PX -0.1515
|
||||
param set-default CA_ROTOR3_PY 0.1875
|
||||
param set-default CA_ROTOR3_KM -0.05
|
||||
param set-default CA_ROTOR4_AX 1.0
|
||||
param set-default CA_ROTOR4_AZ 0.0
|
||||
param set-default CA_ROTOR4_PX 0.2
|
||||
|
||||
param set-default SIM_GZ_EC_FUNC1 101
|
||||
param set-default SIM_GZ_EC_MIN1 0
|
||||
param set-default SIM_GZ_EC_MAX1 1500
|
||||
param set-default SIM_GZ_EC_FUNC2 102
|
||||
param set-default SIM_GZ_EC_MIN2 0
|
||||
param set-default SIM_GZ_EC_MAX2 1500
|
||||
param set-default SIM_GZ_EC_FUNC3 103
|
||||
param set-default SIM_GZ_EC_MIN3 0
|
||||
param set-default SIM_GZ_EC_MAX3 1500
|
||||
param set-default SIM_GZ_EC_FUNC4 104
|
||||
param set-default SIM_GZ_EC_MIN4 0
|
||||
param set-default SIM_GZ_EC_MAX4 1500
|
||||
|
||||
param set-default SIM_GZ_EC_FUNC5 105
|
||||
param set-default SIM_GZ_EC_MIN5 0
|
||||
param set-default SIM_GZ_EC_MAX5 3500
|
||||
|
||||
param set-default SIM_GZ_SV_FUNC1 201
|
||||
param set-default SIM_GZ_SV_FUNC2 202
|
||||
param set-default SIM_GZ_SV_FUNC3 203
|
||||
|
||||
param set-default COM_RC_IN_MODE 1
|
||||
param set-default ASPD_PRIMARY 1
|
||||
|
||||
param set-default CA_SV_CS_COUNT 3
|
||||
param set-default CA_SV_CS0_TYPE 1
|
||||
param set-default CA_SV_CS0_TRQ_R -0.5
|
||||
param set-default CA_SV_CS1_TYPE 2
|
||||
param set-default CA_SV_CS1_TRQ_R 0.5
|
||||
param set-default CA_SV_CS2_TYPE 3
|
||||
param set-default CA_SV_CS2_TRQ_P 1.0
|
||||
|
||||
param set-default FW_L1_PERIOD 12
|
||||
param set-default FW_PR_FF 0.2
|
||||
param set-default FW_PR_P 0.9
|
||||
param set-default FW_PSP_OFF 2
|
||||
param set-default FW_P_LIM_MIN -15
|
||||
param set-default FW_RR_FF 0.1
|
||||
param set-default FW_RR_P 0.3
|
||||
param set-default FW_THR_TRIM 0.25
|
||||
param set-default FW_THR_MAX 0.6
|
||||
param set-default FW_THR_MIN 0.05
|
||||
param set-default FW_T_CLMB_MAX 8
|
||||
param set-default FW_T_SINK_MAX 2.7
|
||||
param set-default FW_T_SINK_MIN 2.2
|
||||
|
||||
param set-default MC_AIRMODE 1
|
||||
param set-default MC_ROLLRATE_P 0.3
|
||||
param set-default MC_YAW_P 1.6
|
||||
|
||||
param set-default MIS_TAKEOFF_ALT 10
|
||||
|
||||
param set-default MPC_ACC_HOR_MAX 2
|
||||
param set-default MPC_XY_P 0.8
|
||||
param set-default MPC_XY_VEL_P_ACC 3
|
||||
param set-default MPC_XY_VEL_I_ACC 4
|
||||
param set-default MPC_XY_VEL_D_ACC 0.1
|
||||
|
||||
param set-default NAV_ACC_RAD 5
|
||||
|
||||
param set-default VT_FWD_THRUST_EN 4
|
||||
param set-default VT_F_TRANS_THR 0.75
|
||||
param set-default VT_B_TRANS_DUR 8
|
||||
param set-default VT_TYPE 2
|
||||
param set-default FD_ESCS_EN 0
|
||||
@@ -73,6 +73,8 @@ px4_add_romfs_files(
|
||||
4001_gz_x500
|
||||
4002_gz_x500_depth
|
||||
4003_gz_rc_cessna
|
||||
4004_gz_standard_vtol
|
||||
4005_gz_foxtech_loong_2160
|
||||
|
||||
6011_gazebo-classic_typhoon_h480
|
||||
6011_gazebo-classic_typhoon_h480.post
|
||||
|
||||
@@ -80,6 +80,7 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
|
||||
sensor_baro_sim start
|
||||
sensor_gps_sim start
|
||||
sensor_mag_sim start
|
||||
sensor_airspeed_sim start
|
||||
|
||||
else
|
||||
echo "ERROR [init] gz_bridge failed to start"
|
||||
@@ -93,6 +94,7 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
|
||||
sensor_baro_sim start
|
||||
sensor_gps_sim start
|
||||
sensor_mag_sim start
|
||||
sensor_airspeed_sim start
|
||||
|
||||
else
|
||||
echo "ERROR [init] gz_bridge failed to start"
|
||||
@@ -107,6 +109,7 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
|
||||
sensor_baro_sim start
|
||||
sensor_gps_sim start
|
||||
sensor_mag_sim start
|
||||
sensor_airspeed_sim start
|
||||
|
||||
else
|
||||
echo "ERROR [init] gz_bridge failed to start"
|
||||
|
||||
File diff suppressed because one or more lines are too long
@@ -0,0 +1,262 @@
|
||||
<?xml version="1.0" encoding="utf-8"?>
|
||||
<COLLADA xmlns="http://www.collada.org/2005/11/COLLADASchema" version="1.4.1">
|
||||
<asset>
|
||||
<contributor>
|
||||
<author/>
|
||||
<authoring_tool>FBX COLLADA exporter</authoring_tool>
|
||||
<comments/>
|
||||
</contributor>
|
||||
<created>2023-01-04T01:05:20Z</created>
|
||||
<keywords/>
|
||||
<modified>2023-01-04T01:05:20Z</modified>
|
||||
<revision/>
|
||||
<subject/>
|
||||
<title/>
|
||||
<unit meter="0.010000" name="centimeter"/>
|
||||
<up_axis>Z_UP</up_axis>
|
||||
</asset>
|
||||
<library_materials>
|
||||
<material id="FBXASC0481FBXASC032-FBXASC032Default" name="FBXASC0481FBXASC032-FBXASC032Default">
|
||||
<instance_effect url="#FBXASC0481FBXASC032-FBXASC032Default-fx"/>
|
||||
</material>
|
||||
</library_materials>
|
||||
<library_effects>
|
||||
<effect id="FBXASC0481FBXASC032-FBXASC032Default-fx" name="FBXASC0481FBXASC032-FBXASC032Default">
|
||||
<profile_COMMON>
|
||||
<technique sid="standard">
|
||||
<phong>
|
||||
<emission>
|
||||
<color sid="emission">0.000000 0.000000 0.000000 1.000000</color>
|
||||
</emission>
|
||||
<ambient>
|
||||
<color sid="ambient">0.588235 0.588235 0.588235 1.000000</color>
|
||||
</ambient>
|
||||
<diffuse>
|
||||
<color sid="diffuse">0.588235 0.588235 0.588235 1.000000</color>
|
||||
</diffuse>
|
||||
<specular>
|
||||
<color sid="specular">0.486000 0.486000 0.486000 1.000000</color>
|
||||
</specular>
|
||||
<shininess>
|
||||
<float sid="shininess">2.000000</float>
|
||||
</shininess>
|
||||
<reflective>
|
||||
<color sid="reflective">0.000000 0.000000 0.000000 1.000000</color>
|
||||
</reflective>
|
||||
<reflectivity>
|
||||
<float sid="reflectivity">1.000000</float>
|
||||
</reflectivity>
|
||||
<transparent opaque="RGB_ZERO">
|
||||
<color sid="transparent">1.000000 1.000000 1.000000 1.000000</color>
|
||||
</transparent>
|
||||
<transparency>
|
||||
<float sid="transparency">0.000000</float>
|
||||
</transparency>
|
||||
</phong>
|
||||
</technique>
|
||||
</profile_COMMON>
|
||||
</effect>
|
||||
</library_effects>
|
||||
<library_geometries>
|
||||
<geometry id="aileron_left-lib" name="aileron_leftMesh">
|
||||
<mesh>
|
||||
<source id="aileron_left-POSITION">
|
||||
<float_array id="aileron_left-POSITION-array" count="48">
|
||||
-8.508881 -8.085777 -0.718638
|
||||
-8.508881 -8.085783 -0.353647
|
||||
4.939667 -6.844479 -0.718638
|
||||
4.939667 -6.844481 -0.353647
|
||||
-17.070042 -8.085783 -0.353647
|
||||
-17.070042 -8.085777 -0.718638
|
||||
17.070045 -4.887245 -0.718638
|
||||
17.070038 -4.887245 -0.353647
|
||||
-8.508881 0.511266 -0.718638
|
||||
-8.508881 0.511267 0.718638
|
||||
4.939667 0.511266 -0.718638
|
||||
4.939667 0.511266 0.642922
|
||||
-17.070042 0.511266 -0.718638
|
||||
-17.070042 0.511266 0.718212
|
||||
17.070045 0.511266 -0.718638
|
||||
17.070030 0.511267 0.494327
|
||||
</float_array>
|
||||
<technique_common>
|
||||
<accessor source="#aileron_left-POSITION-array" count="16" stride="3">
|
||||
<param name="X" type="float"/>
|
||||
<param name="Y" type="float"/>
|
||||
<param name="Z" type="float"/>
|
||||
</accessor>
|
||||
</technique_common>
|
||||
</source>
|
||||
<source id="aileron_left-Normal0">
|
||||
<float_array id="aileron_left-Normal0-array" count="252">
|
||||
0.004350 -0.126175 0.991998
|
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0.012806 -0.135273 0.990726
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0.013164 -0.135857 0.990641
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0.012806 -0.135273 0.990726
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0.004350 -0.126175 0.991998
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|
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0.046003 -0.998941 -0.000013
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0.125672 -0.992072 -0.000006
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0.125672 -0.992072 -0.000006
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0.046003 -0.998941 -0.000013
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0.046003 -0.998941 -0.000013
|
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0.013164 -0.135857 0.990641
|
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0.017606 -0.143110 0.989550
|
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0.017606 -0.143110 0.989550
|
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0.017606 -0.143110 0.989550
|
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0.013164 -0.135857 0.990641
|
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0.012806 -0.135273 0.990726
|
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0.125672 -0.992072 -0.000006
|
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0.159290 -0.987232 -0.000001
|
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0.125672 -0.992072 -0.000006
|
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-0.000025 -0.123744 0.992314
|
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0.004220 -0.126103 0.992008
|
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0.004350 -0.126175 0.991998
|
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0.004220 -0.126103 0.992008
|
||||
-0.000025 -0.123744 0.992314
|
||||
-0.000025 -0.123744 0.992314
|
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0.000000 -1.000000 -0.000016
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0.046003 -0.998941 -0.000013
|
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0.046003 -0.998941 -0.000013
|
||||
0.046003 -0.998941 -0.000013
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0.000000 -1.000000 -0.000016
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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0.000000 0.000000 -1.000000
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|
||||
<input semantic="NORMAL" offset="1" source="#Object004-Normal0"/>
|
||||
<input semantic="TEXCOORD" offset="2" set="0" source="#Object004-UV0"/>
|
||||
<p> 1 0 1 4 1 6 15 2 27 4 3 6 1 4 1 3 5 4 15 6 27 14 7 26 1 8 1 1 9 2 2 10 3 3 11 5 2 12 3 1 13 2 0 14 0 9 15 16 2 16 3 8 17 14 2 18 3 9 19 16 3 20 5 7 21 11 5 22 7 17 23 29 5 24 7 16 25 28 17 26 29 6 27 10 5 28 7 7 29 11 2 30 12 0 31 8 5 32 9 2 33 12 5 34 9 6 35 13 8 36 15 2 37 12 6 38 13 8 39 15 6 40 13 10 41 18 7 42 11 19 43 31 10 44 19 10 45 19 6 46 10 7 47 11 19 48 31 7 49 11 17 50 29 14 51 26 20 52 32 11 53 20 14 54 26 11 55 20 1 56 1 11 57 21 0 58 0 1 59 2 0 60 0 11 61 21 12 62 22 0 63 8 13 64 25 5 65 9 13 66 25 0 67 8 12 68 23 18 69 30 4 70 6 9 71 17 3 72 4 9 73 17 4 74 6 4 75 6 18 76 30 15 77 27 13 78 24 16 79 28 5 80 7 16 81 28 13 82 24 21 83 33 10 84 10 19 85 19 9 86 9 18 87 18 9 88 9 19 89 19 19 90 19 17 91 17 18 92 18 15 93 15 18 94 18 17 95 17 17 96 17 14 97 14 15 98 15 14 99 14 17 100 17 16 101 16 16 102 16 21 103 21 14 104 14 20 105 20 14 106 14 21 107 21 21 108 21 11 109 11 20 110 20 11 111 11 21 112 21 13 113 13</p>
|
||||
</triangles>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</library_geometries>
|
||||
<library_visual_scenes>
|
||||
<visual_scene id="Object004" name="Object004">
|
||||
<node name="Object004" id="Object004" sid="Object004">
|
||||
<matrix sid="matrix">-0.000000 0.000000 0.287929 0.000000 0.000000 0.280290 -0.000000 0.000000 0.280290 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 1.000000</matrix>
|
||||
<instance_geometry url="#Object004-lib">
|
||||
<bind_material>
|
||||
<technique_common>
|
||||
<instance_material symbol="FBXASC0481FBXASC032-FBXASC032Default" target="#FBXASC0481FBXASC032-FBXASC032Default"/>
|
||||
</technique_common>
|
||||
</bind_material>
|
||||
</instance_geometry>
|
||||
<extra>
|
||||
<technique profile="FCOLLADA">
|
||||
<visibility>1.000000</visibility>
|
||||
</technique>
|
||||
</extra>
|
||||
</node>
|
||||
<extra>
|
||||
<technique profile="MAX3D">
|
||||
<frame_rate>30.000000</frame_rate>
|
||||
</technique>
|
||||
<technique profile="FCOLLADA">
|
||||
<start_time>0.000000</start_time>
|
||||
<end_time>3.333333</end_time>
|
||||
</technique>
|
||||
</extra>
|
||||
</visual_scene>
|
||||
</library_visual_scenes>
|
||||
<scene>
|
||||
<instance_visual_scene url="#Object004"/>
|
||||
</scene>
|
||||
</COLLADA>
|
||||
@@ -0,0 +1,15 @@
|
||||
<?xml version="1.0"?>
|
||||
<model>
|
||||
<name>foxtech_loong_2160</name>
|
||||
<version>1.0</version>
|
||||
<sdf version='1.10'>model.sdf</sdf>
|
||||
|
||||
<author>
|
||||
<name>Alejandro Hernandez Cordero</name>
|
||||
<email>alejandro@OpenRobotics.org</email>
|
||||
</author>
|
||||
|
||||
<description>
|
||||
This is a model of a VTOL.
|
||||
</description>
|
||||
</model>
|
||||
@@ -0,0 +1,736 @@
|
||||
<?xml version="1.0"?>
|
||||
<sdf version="1.10">
|
||||
<model name='foxtech_loong_2160'>
|
||||
<pose>0 0 0.5 0 0 0</pose>
|
||||
<link name="base_link">
|
||||
<visual name="visual_base_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/VTOL.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<collision name='base_link_collision'>
|
||||
<pose>0 0 -0.07 0 0 0</pose>
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.55 2.144 0.05</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<kp>100000</kp>
|
||||
<kd>1.0</kd>
|
||||
<max_vel>0.1</max_vel>
|
||||
<min_depth>0.001</min_depth>
|
||||
</ode>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
<inertial>
|
||||
<pose>-0.13220955077769075 -4.9142356489896525e-08 0.04102678265168308 1.5707963267948966 -1.5231416433972742 0</pose>
|
||||
<mass>3.584838964525901</mass>
|
||||
<inertia>
|
||||
<ixx>0.67738485351961117</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.40350427325261343</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.28925142846350795</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<sensor name="imu_sensor" type="imu">
|
||||
<always_on>1</always_on>
|
||||
<update_rate>250</update_rate>
|
||||
</sensor>
|
||||
</link>
|
||||
<link name="legs_link">
|
||||
<pose>0 0 0 0 0 -1.57</pose>
|
||||
<visual name="visual_legs_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/legs.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
<material>
|
||||
<ambient>1 1 1 1.0</ambient>
|
||||
<diffuse>1 1 1 1.0</diffuse>
|
||||
</material>
|
||||
</visual>
|
||||
<inertial>
|
||||
<pose>3.7153930608820144e-06 -0.17032952180315669 -0.067888027893133446 0.010363008330798451 -1.494594844601834 1.5602561510969915</pose>
|
||||
<mass>0.6675493726413797</mass>
|
||||
<inertia>
|
||||
<ixx>0.032153703643267112</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.031670484418576728</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.00069030434527976208</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<!-- <collision name="collision_legs_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/legs.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
</link>
|
||||
<joint name='legs_joint' type='fixed'>
|
||||
<child>legs_link</child>
|
||||
<parent>base_link</parent>
|
||||
</joint>
|
||||
<link name="aileron_left_link">
|
||||
<pose>-0.122 0.713 0.062 0 0 -1.57</pose>
|
||||
<visual name="visual_aileron_left_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/aileron_left.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<!-- <collision name="collision_aileron_left_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/aileron_left.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
<inertial>
|
||||
<pose>0.016428520956860652 -0.026006344294799606 -0.0023574007803185606 -1.5395303459623877 -1.5044452951949348 -1.6400967799666224</pose>
|
||||
<mass>0.48889497715279695</mass>
|
||||
<inertia>
|
||||
<ixx>0.0046714785213929121</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.0044549919806967505</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.00022471747503113157</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
</link>
|
||||
<joint name="servo_0" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>aileron_left_link</child>
|
||||
<axis>
|
||||
<xyz>-1 0 0</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="aileron_right_link">
|
||||
<pose>-0.122 -0.713 0.062 0 0 -1.57</pose>
|
||||
<visual name="visual_aileron_right_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/aileron_right.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<!-- <collision name="collision_aileron_right_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/aileron_right.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
<inertial>
|
||||
<pose>-0.016428520373255796 -0.026006344259039589 -0.0023573984798765397 -1.6020624043352432 -1.5044453783967096 -1.5014957739781367</pose>
|
||||
<mass>0.48889496879062661</mass>
|
||||
<inertia>
|
||||
<ixx>0.0046714784977765411</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.0044549919610427299</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.00022471747055809963</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
</link>
|
||||
<joint name="servo_1" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>aileron_right_link</child>
|
||||
<axis>
|
||||
<xyz>-1 0 0</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="elevator_link">
|
||||
<visual name="visual_elevator_right_link">
|
||||
<pose>-0.883 -0.145 0.058 0 0 -1.57</pose>
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/elevator_right.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<!-- <collision name="collision_elevator_right_link">
|
||||
<pose>-0.883 -0.145 0.058 0 0 -1.57</pose>
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/elevator_right.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
<visual name="visual_elevator_left_link">
|
||||
<pose>-0.883 0.145 0.058 0 0 -1.57</pose>
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/elevator_left.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<!-- <collision name="collision_elevator_left_link">
|
||||
<pose>-0.883 0.145 0.058 0 0 -1.57</pose>
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/elevator_left.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
<inertial>
|
||||
<pose>-0.90103043712540809 -1.4356019912623529e-05 0.057304774890379953 -1.5708004219891478 -1.5333831628670098 -3.141493135229823</pose>
|
||||
<mass>0.12150608610187363</mass>
|
||||
<inertia>
|
||||
<ixx>0.0029053735939891879</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.0028879706692375028</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>1.7683703559870421e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
</link>
|
||||
<joint name="servo_2" type="revolute">
|
||||
<pose>-0.883 0 0.058 0 0 -1.57</pose>
|
||||
<parent>base_link</parent>
|
||||
<child>elevator_link</child>
|
||||
<axis>
|
||||
<xyz>-1 0 0</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="rudder_link">
|
||||
<pose>-0.887 0 0.201 0 0 -1.57</pose>
|
||||
<visual name="visual_rudder_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/rudder.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<!-- <collision name="collision_rudder_link">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/rudder.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</collision> -->
|
||||
<inertial>p
|
||||
<pose>3.0720176589210631e-09 -0.014597633583934367 -0.00023793299837082617 -0.00096325055376496349 0 0</pose>
|
||||
<mass>0.08686124232617691</mass>
|
||||
<inertia>
|
||||
<ixx>0.00029239473616759126</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.00028035840542611708</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>1.2453403617197103e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
</link>
|
||||
<joint name="servo_3" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>rudder_link</child>
|
||||
<axis>
|
||||
<xyz>0 0 1</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="rotor_3">
|
||||
<gravity>true</gravity>
|
||||
<self_collide>false</self_collide>
|
||||
<velocity_decay/>
|
||||
<pose>-0.403 -0.427 0.083 0 0 -1.57</pose>
|
||||
<inertial>
|
||||
<mass>0.016076923076923075</mass>
|
||||
<inertia>
|
||||
<ixx>3.8464910483993325e-07</ixx>
|
||||
<iyy>2.6115851691700804e-05</iyy>
|
||||
<izz>2.649858234714004e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<visual name="rotor_3_visual">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/propeller_ccw.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<collision name="rotor_3_collision">
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<min_depth>0.001</min_depth>
|
||||
<max_vel>0</max_vel>
|
||||
</ode>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
</link>
|
||||
<joint name="rotor_0_joint" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>rotor_0</child>
|
||||
<axis>
|
||||
<xyz>0 0 1</xyz>
|
||||
<limit>
|
||||
<lower>-1e+16</lower>
|
||||
<upper>1e+16</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<spring_reference>0</spring_reference>
|
||||
<spring_stiffness>0</spring_stiffness>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="rotor_2">
|
||||
<gravity>true</gravity>
|
||||
<self_collide>false</self_collide>
|
||||
<velocity_decay/>
|
||||
<pose>0.403 0.427 0.083 0 0 -1.57</pose>
|
||||
<inertial>
|
||||
<mass>0.016076923076923075</mass>
|
||||
<inertia>
|
||||
<ixx>3.8464910483993325e-07</ixx>
|
||||
<iyy>2.6115851691700804e-05</iyy>
|
||||
<izz>2.649858234714004e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<visual name="rotor_2_visual">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/propeller_ccw.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<collision name="rotor_2_collision">
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<min_depth>0.001</min_depth>
|
||||
<max_vel>0</max_vel>
|
||||
</ode>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
</link>
|
||||
<joint name="rotor_1_joint" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>rotor_1</child>
|
||||
<axis>
|
||||
<xyz>0 0 1</xyz>
|
||||
<limit>
|
||||
<lower>-1e+16</lower>
|
||||
<upper>1e+16</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<spring_reference>0</spring_reference>
|
||||
<spring_stiffness>0</spring_stiffness>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="rotor_0">
|
||||
<gravity>true</gravity>
|
||||
<self_collide>false</self_collide>
|
||||
<velocity_decay/>
|
||||
<pose>0.403 -0.427 0.083 0 0 -1.57</pose>
|
||||
<inertial>
|
||||
<mass>0.016076923076923075</mass>
|
||||
<inertia>
|
||||
<ixx>3.8464910483993325e-07</ixx>
|
||||
<iyy>2.6115851691700804e-05</iyy>
|
||||
<izz>2.649858234714004e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<visual name="rotor_0_visual">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/propeller_cw.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<collision name="rotor_0_collision">
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<min_depth>0.001</min_depth>
|
||||
<max_vel>0</max_vel>
|
||||
</ode>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
</link>
|
||||
<joint name="rotor_2_joint" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>rotor_2</child>
|
||||
<axis>
|
||||
<xyz>0 0 1</xyz>
|
||||
<limit>
|
||||
<lower>-1e+16</lower>
|
||||
<upper>1e+16</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<spring_reference>0</spring_reference>
|
||||
<spring_stiffness>0</spring_stiffness>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name="rotor_1">
|
||||
<gravity>true</gravity>
|
||||
<self_collide>false</self_collide>
|
||||
<velocity_decay/>
|
||||
<pose>-0.403 0.427 0.083 0 0 -1.57</pose>
|
||||
<inertial>
|
||||
<mass>0.016076923076923075</mass>
|
||||
<inertia>
|
||||
<ixx>3.8464910483993325e-07</ixx>
|
||||
<iyy>2.6115851691700804e-05</iyy>
|
||||
<izz>2.649858234714004e-05</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<visual name="rotor_1_visual">
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/propeller_cw.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<collision name="rotor_1_collision">
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.2792307692307692 0.016923076923076923 0.0008461538461538462</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<min_depth>0.001</min_depth>
|
||||
<max_vel>0</max_vel>
|
||||
</ode>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
</link>
|
||||
<joint name="rotor_3_joint" type="revolute">
|
||||
<parent>base_link</parent>
|
||||
<child>rotor_3</child>
|
||||
<axis>
|
||||
<xyz>0 0 1</xyz>
|
||||
<limit>
|
||||
<lower>-1e+16</lower>
|
||||
<upper>1e+16</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<spring_reference>0</spring_reference>
|
||||
<spring_stiffness>0</spring_stiffness>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
<link name='rotor_puller'>
|
||||
<pose>0.379 0.0 0.0 -1.57 1.57 -1.57</pose>
|
||||
<inertial>
|
||||
<pose>0 0 0 0 0 0</pose>
|
||||
<mass>0.005</mass>
|
||||
<inertia>
|
||||
<ixx>9.75e-07</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.000166704</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.000167604</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<collision name='rotor_puller_collision'>
|
||||
<geometry>
|
||||
<cylinder>
|
||||
<length>0.005</length>
|
||||
<radius>0.06</radius>
|
||||
</cylinder>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode/>
|
||||
</contact>
|
||||
<friction>
|
||||
<ode/>
|
||||
</friction>
|
||||
</surface>
|
||||
</collision>
|
||||
<visual name='rotor_puller_visual'>
|
||||
<geometry>
|
||||
<mesh>
|
||||
<uri>model://foxtech_loong_2160/meshes/propeller_cw.dae</uri>
|
||||
</mesh>
|
||||
</geometry>
|
||||
</visual>
|
||||
<gravity>1</gravity>
|
||||
<velocity_decay/>
|
||||
<self_collide>0</self_collide>
|
||||
</link>
|
||||
<joint name='rotor_puller_joint' type='revolute'>
|
||||
<pose>0.0 0 0.0 0 -1.57 0</pose>
|
||||
<child>rotor_puller</child>
|
||||
<parent>base_link</parent>
|
||||
<axis>
|
||||
<xyz>1 0 0</xyz>
|
||||
<limit>
|
||||
<lower>-1e+16</lower>
|
||||
<upper>1e+16</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<spring_reference>0</spring_reference>
|
||||
<spring_stiffness>0</spring_stiffness>
|
||||
</dynamics>
|
||||
</axis>
|
||||
</joint>
|
||||
|
||||
<plugin filename="gz-sim-multicopter-motor-model-system" name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_0_joint</jointName>
|
||||
<linkName>rotor_0</linkName>
|
||||
<turningDirection>ccw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>0</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<!-- <plugin name='back_left_motor_model' filename='libgazebo_motor_model.so'> -->
|
||||
<plugin filename="gz-sim-multicopter-motor-model-system" name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_1_joint</jointName>
|
||||
<linkName>rotor_1</linkName>
|
||||
<turningDirection>ccw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>1</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_2_joint</jointName>
|
||||
<linkName>rotor_2</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>2</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_3_joint</jointName>
|
||||
<linkName>rotor_3</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>3</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_puller_joint</jointName>
|
||||
<linkName>rotor_puller</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>3500</maxRotVelocity>
|
||||
<motorConstant>8.54858e-06</motorConstant>
|
||||
<momentConstant>0.01</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>4</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>0.05984281113</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.05 0.45 0.05</cp>
|
||||
<area>0.6</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_0</control_joint_name>
|
||||
<control_joint_rad_to_cl>-0.3</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_0</joint_name>
|
||||
<sub_topic>servo_0</sub_topic>
|
||||
<p_gain>10.0</p_gain>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>0.05984281113</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.05 -0.45 0.05</cp>
|
||||
<area>0.6</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_1</control_joint_name>
|
||||
<control_joint_rad_to_cl>-0.3</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_1</joint_name>
|
||||
<sub_topic>servo_1</sub_topic>
|
||||
<p_gain>10.0</p_gain>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>-0.2</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.5 0 0</cp>
|
||||
<area>0.01</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_2</control_joint_name>
|
||||
<control_joint_rad_to_cl>-4.0</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_2</joint_name>
|
||||
<sub_topic>servo_2</sub_topic>
|
||||
<p_gain>10.0</p_gain>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>0.0</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0.</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.5 0 0.05</cp>
|
||||
<area>0.02</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 1 0</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_3</control_joint_name>
|
||||
<control_joint_rad_to_cl>0.8</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_3</joint_name>
|
||||
<sub_topic>servo_3</sub_topic>
|
||||
<p_gain>10.0</p_gain>
|
||||
</plugin>
|
||||
</model>
|
||||
</sdf>
|
||||
File diff suppressed because one or more lines are too long
File diff suppressed because one or more lines are too long
File diff suppressed because one or more lines are too long
File diff suppressed because one or more lines are too long
File diff suppressed because one or more lines are too long
@@ -0,0 +1,15 @@
|
||||
<?xml version="1.0"?>
|
||||
<model>
|
||||
<name>Standard VTOL</name>
|
||||
<version>1.0</version>
|
||||
<sdf version='1.10'>model.sdf</sdf>
|
||||
|
||||
<author>
|
||||
<name>Roman Bapst</name>
|
||||
<email>roman@px4.io</email>
|
||||
</author>
|
||||
|
||||
<description>
|
||||
This is a model of a standard VTOL quad plane.
|
||||
</description>
|
||||
</model>
|
||||
@@ -0,0 +1,748 @@
|
||||
<?xml version="1.0"?>
|
||||
<!-- DO NOT EDIT: Generated from standard_vtol.sdf.jinja -->
|
||||
<sdf version='1.10'>
|
||||
<model name='standard_vtol'>
|
||||
<pose>0 0 0.246 0 0 0</pose>
|
||||
<link name='base_link'>
|
||||
<pose>0 0 0 0 0 0</pose>
|
||||
<inertial>
|
||||
<pose>0 0 0 0 0 0</pose>
|
||||
<mass>5</mass>
|
||||
<inertia>
|
||||
<ixx>0.477708333333</ixx>
|
||||
<ixy>0</ixy>
|
||||
<ixz>0</ixz>
|
||||
<iyy>0.341666666667</iyy>
|
||||
<iyz>0</iyz>
|
||||
<izz>0.811041666667</izz>
|
||||
</inertia>
|
||||
</inertial>
|
||||
<collision name='base_link_collision'>
|
||||
<pose>0 0 -0.07 0 0 0</pose>
|
||||
<geometry>
|
||||
<box>
|
||||
<size>0.55 2.144 0.05</size>
|
||||
</box>
|
||||
</geometry>
|
||||
<surface>
|
||||
<contact>
|
||||
<ode>
|
||||
<kp>100000</kp>
|
||||
<kd>1.0</kd>
|
||||
<max_vel>0.1</max_vel>
|
||||
<min_depth>0.001</min_depth>
|
||||
</ode>
|
||||
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||||
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|
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|
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|
||||
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||||
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|
||||
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||||
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|
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|
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|
||||
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|
||||
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|
||||
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|
||||
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||||
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||||
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|
||||
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|
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|
||||
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|
||||
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|
||||
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||||
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||||
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|
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|
||||
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|
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|
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|
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|
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|
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|
||||
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|
||||
<ixx>0.000001</ixx>
|
||||
<ixy>0.0</ixy>
|
||||
<iyy>0.000001</iyy>
|
||||
<ixz>0.0</ixz>
|
||||
<iyz>0.0</iyz>
|
||||
<izz>0.000001</izz>
|
||||
</inertia>
|
||||
<pose> -0.5 0 0 0.00 0 0.0</pose>
|
||||
</inertial>
|
||||
</link>
|
||||
<joint name='servo_0' type='revolute'>
|
||||
<parent>base_link</parent>
|
||||
<child>left_elevon</child>
|
||||
<pose>-0.18 0.6 -0.005 0 0 0.265</pose>
|
||||
<axis>
|
||||
<xyz>0 1 0</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
<physics>
|
||||
<ode>
|
||||
<implicit_spring_damper>1</implicit_spring_damper>
|
||||
</ode>
|
||||
</physics>
|
||||
</joint>
|
||||
<joint name='servo_1' type='revolute'>
|
||||
<parent>base_link</parent>
|
||||
<child>right_elevon</child>
|
||||
<pose>-0.18 -0.6 -0.005 0 0 -0.265</pose>
|
||||
<axis>
|
||||
<xyz>0 1 0</xyz>
|
||||
<limit>
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
<physics>
|
||||
<ode>
|
||||
<implicit_spring_damper>1</implicit_spring_damper>
|
||||
</ode>
|
||||
</physics>
|
||||
</joint>
|
||||
<joint name='servo_2' type='revolute'>
|
||||
<parent>base_link</parent>
|
||||
<child>elevator</child>
|
||||
<pose> -0.5 0 0 0 0 0</pose>
|
||||
<axis>
|
||||
<xyz>0 1 0</xyz>
|
||||
<limit>
|
||||
<!-- -30/+30 deg. -->
|
||||
<lower>-0.53</lower>
|
||||
<upper>0.53</upper>
|
||||
</limit>
|
||||
<dynamics>
|
||||
<damping>1.000</damping>
|
||||
</dynamics>
|
||||
</axis>
|
||||
<physics>
|
||||
<ode>
|
||||
<implicit_spring_damper>1</implicit_spring_damper>
|
||||
</ode>
|
||||
</physics>
|
||||
</joint>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>0.05984281113</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.05 0.3 0.05</cp>
|
||||
<area>0.50</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_0</control_joint_name>
|
||||
<control_joint_rad_to_cl>-1.0</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_0</joint_name>
|
||||
<sub_topic>servo_0</sub_topic>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>0.05984281113</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.05 -0.3 0.05</cp>
|
||||
<area>0.50</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_1</control_joint_name>
|
||||
<control_joint_rad_to_cl>-1.0</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_1</joint_name>
|
||||
<sub_topic>servo_1</sub_topic>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-lift-drag-system" name="gz::sim::systems::LiftDrag">
|
||||
<a0>-0.2</a0>
|
||||
<cla>4.752798721</cla>
|
||||
<cda>0.6417112299</cda>
|
||||
<cma>0.0</cma>
|
||||
<alpha_stall>0.3391428111</alpha_stall>
|
||||
<cla_stall>-3.85</cla_stall>
|
||||
<cda_stall>-0.9233984055</cda_stall>
|
||||
<cma_stall>0</cma_stall>
|
||||
<cp>-0.5 0 0</cp>
|
||||
<area>0.01</area>
|
||||
<air_density>1.2041</air_density>
|
||||
<forward>1 0 0</forward>
|
||||
<upward>0 0 1</upward>
|
||||
<link_name>base_link</link_name>
|
||||
<control_joint_name>servo_2</control_joint_name>
|
||||
<control_joint_name>servo_2</control_joint_name>
|
||||
<control_joint_rad_to_cl>-12.0</control_joint_rad_to_cl>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
|
||||
<joint_name>servo_2</joint_name>
|
||||
<sub_topic>servo_2</sub_topic>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-multicopter-motor-model-system" name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_0_joint</jointName>
|
||||
<linkName>rotor_0</linkName>
|
||||
<turningDirection>ccw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>0</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin filename="gz-sim-multicopter-motor-model-system" name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_1_joint</jointName>
|
||||
<linkName>rotor_1</linkName>
|
||||
<turningDirection>ccw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>1</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_2_joint</jointName>
|
||||
<linkName>rotor_2</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>2</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_3_joint</jointName>
|
||||
<linkName>rotor_3</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>1500</maxRotVelocity>
|
||||
<motorConstant>2e-05</motorConstant>
|
||||
<momentConstant>0.06</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>3</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<plugin
|
||||
filename="gz-sim-multicopter-motor-model-system"
|
||||
name="gz::sim::systems::MulticopterMotorModel">
|
||||
<jointName>rotor_puller_joint</jointName>
|
||||
<linkName>rotor_puller</linkName>
|
||||
<turningDirection>cw</turningDirection>
|
||||
<timeConstantUp>0.0125</timeConstantUp>
|
||||
<timeConstantDown>0.025</timeConstantDown>
|
||||
<maxRotVelocity>3500</maxRotVelocity>
|
||||
<motorConstant>8.54858e-06</motorConstant>
|
||||
<momentConstant>0.01</momentConstant>
|
||||
<commandSubTopic>command/motor_speed</commandSubTopic>
|
||||
<motorNumber>4</motorNumber>
|
||||
<rotorDragCoefficient>0.000106428</rotorDragCoefficient>
|
||||
<rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
|
||||
<rotorVelocitySlowdownSim>20</rotorVelocitySlowdownSim>
|
||||
<motorType>velocity</motorType>
|
||||
</plugin>
|
||||
<static>0</static>
|
||||
</model>
|
||||
</sdf>
|
||||
@@ -4,6 +4,7 @@ menu "Simulation"
|
||||
default n
|
||||
select MODULES_SIMULATION_BATTERY_SIMULATOR
|
||||
select MODULES_SIMULATION_PWM_OUT_SIM
|
||||
select MODULES_SIMULATION_SENSOR_AIRSPEED_SIM
|
||||
select MODULES_SIMULATION_SENSOR_BARO_SIM
|
||||
select MODULES_SIMULATION_SENSOR_GPS_SIM
|
||||
select MODULES_SIMULATION_SENSOR_MAG_SIM
|
||||
|
||||
@@ -185,6 +185,7 @@ int GZBridge::task_spawn(int argc, char *argv[])
|
||||
const char *model_pose = nullptr;
|
||||
const char *model_sim = nullptr;
|
||||
const char *px4_instance = nullptr;
|
||||
std::string model_name_std;
|
||||
|
||||
|
||||
bool error_flag = false;
|
||||
@@ -248,7 +249,7 @@ int GZBridge::task_spawn(int argc, char *argv[])
|
||||
}
|
||||
|
||||
} else if (!model_name) {
|
||||
std::string model_name_std = std::string(model_sim) + "_" + std::string(px4_instance);
|
||||
model_name_std = std::string(model_sim) + "_" + std::string(px4_instance);
|
||||
model_name = model_name_std.c_str();
|
||||
}
|
||||
|
||||
|
||||
@@ -0,0 +1,43 @@
|
||||
############################################################################
|
||||
#
|
||||
# Copyright (c) 2021-2022 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_module(
|
||||
MODULE modules__simulation__sensor_airspeed_sim
|
||||
MAIN sensor_airspeed_sim
|
||||
COMPILE_FLAGS
|
||||
SRCS
|
||||
SensorAirspeedSim.cpp
|
||||
SensorAirspeedSim.hpp
|
||||
DEPENDS
|
||||
px4_work_queue
|
||||
)
|
||||
@@ -0,0 +1,5 @@
|
||||
menuconfig MODULES_SIMULATION_SENSOR_AIRSPEED_SIM
|
||||
bool "sensor_airspeed_sim"
|
||||
default n
|
||||
---help---
|
||||
Enable support for sensor_airspeed_sim
|
||||
@@ -0,0 +1,206 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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 "SensorAirspeedSim.hpp"
|
||||
|
||||
#include <drivers/drv_sensor.h>
|
||||
#include <lib/drivers/device/Device.hpp>
|
||||
#include <lib/geo/geo.h>
|
||||
|
||||
using namespace matrix;
|
||||
|
||||
SensorAirspeedSim::SensorAirspeedSim() :
|
||||
ModuleParams(nullptr),
|
||||
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::hp_default)
|
||||
{
|
||||
}
|
||||
|
||||
SensorAirspeedSim::~SensorAirspeedSim()
|
||||
{
|
||||
perf_free(_loop_perf);
|
||||
}
|
||||
|
||||
bool SensorAirspeedSim::init()
|
||||
{
|
||||
ScheduleOnInterval(125_ms); // 8 Hz
|
||||
return true;
|
||||
}
|
||||
|
||||
float SensorAirspeedSim::generate_wgn()
|
||||
{
|
||||
// generate white Gaussian noise sample with std=1
|
||||
|
||||
// algorithm 1:
|
||||
// float temp=((float)(rand()+1))/(((float)RAND_MAX+1.0f));
|
||||
// return sqrtf(-2.0f*logf(temp))*cosf(2.0f*M_PI_F*rand()/RAND_MAX);
|
||||
// algorithm 2: from BlockRandGauss.hpp
|
||||
static float V1, V2, S;
|
||||
static bool phase = true;
|
||||
float X;
|
||||
|
||||
if (phase) {
|
||||
do {
|
||||
float U1 = (float)rand() / (float)RAND_MAX;
|
||||
float U2 = (float)rand() / (float)RAND_MAX;
|
||||
V1 = 2.0f * U1 - 1.0f;
|
||||
V2 = 2.0f * U2 - 1.0f;
|
||||
S = V1 * V1 + V2 * V2;
|
||||
} while (S >= 1.0f || fabsf(S) < 1e-8f);
|
||||
|
||||
X = V1 * float(sqrtf(-2.0f * float(logf(S)) / S));
|
||||
|
||||
} else {
|
||||
X = V2 * float(sqrtf(-2.0f * float(logf(S)) / S));
|
||||
}
|
||||
|
||||
phase = !phase;
|
||||
return X;
|
||||
}
|
||||
|
||||
void SensorAirspeedSim::Run()
|
||||
{
|
||||
if (should_exit()) {
|
||||
ScheduleClear();
|
||||
exit_and_cleanup();
|
||||
return;
|
||||
}
|
||||
|
||||
perf_begin(_loop_perf);
|
||||
|
||||
// Check if parameters have changed
|
||||
if (_parameter_update_sub.updated()) {
|
||||
// clear update
|
||||
parameter_update_s param_update;
|
||||
_parameter_update_sub.copy(¶m_update);
|
||||
|
||||
updateParams();
|
||||
}
|
||||
|
||||
if (_vehicle_local_position_sub.updated() && _vehicle_global_position_sub.updated()
|
||||
&& _vehicle_attitude_sub.updated()) {
|
||||
|
||||
vehicle_local_position_s lpos{};
|
||||
_vehicle_local_position_sub.copy(&lpos);
|
||||
|
||||
vehicle_global_position_s gpos{};
|
||||
_vehicle_global_position_sub.copy(&gpos);
|
||||
|
||||
vehicle_attitude_s attitude{};
|
||||
_vehicle_attitude_sub.copy(&attitude);
|
||||
|
||||
Vector3f local_velocity = Vector3f{lpos.vx, lpos.vy, lpos.vz};
|
||||
Vector3f body_velocity = Dcmf{Quatf{attitude.q}} .transpose() * local_velocity;
|
||||
|
||||
// device id
|
||||
device::Device::DeviceId device_id;
|
||||
device_id.devid_s.bus_type = device::Device::DeviceBusType::DeviceBusType_SIMULATION;
|
||||
device_id.devid_s.bus = 0;
|
||||
device_id.devid_s.address = 0;
|
||||
device_id.devid_s.devtype = DRV_DIFF_PRESS_DEVTYPE_SIM;
|
||||
|
||||
const float alt_amsl = gpos.alt;
|
||||
const float temperature_local = TEMPERATURE_MSL - LAPSE_RATE * alt_amsl;
|
||||
const float density_ratio = powf(TEMPERATURE_MSL / temperature_local, 4.256f);
|
||||
const float air_density = AIR_DENSITY_MSL / density_ratio;
|
||||
|
||||
// calculate differential pressure + noise in hPa
|
||||
const float diff_pressure_noise = (float)generate_wgn() * 0.01f;
|
||||
float diff_pressure = sign(body_velocity(0)) * 0.005f * air_density * body_velocity(0) * body_velocity(
|
||||
0) + diff_pressure_noise;
|
||||
|
||||
|
||||
differential_pressure_s differential_pressure{};
|
||||
// report.timestamp_sample = time;
|
||||
differential_pressure.device_id = 1377548; // 1377548: DRV_DIFF_PRESS_DEVTYPE_SIM, BUS: 1, ADDR: 5, TYPE: SIMULATION
|
||||
differential_pressure.differential_pressure_pa = (double)diff_pressure * 100.0; // hPa to Pa;
|
||||
differential_pressure.temperature = temperature_local;
|
||||
differential_pressure.timestamp = hrt_absolute_time();
|
||||
_differential_pressure_pub.publish(differential_pressure);
|
||||
|
||||
}
|
||||
|
||||
perf_end(_loop_perf);
|
||||
}
|
||||
|
||||
int SensorAirspeedSim::task_spawn(int argc, char *argv[])
|
||||
{
|
||||
SensorAirspeedSim *instance = new SensorAirspeedSim();
|
||||
|
||||
if (instance) {
|
||||
_object.store(instance);
|
||||
_task_id = task_id_is_work_queue;
|
||||
|
||||
if (instance->init()) {
|
||||
return PX4_OK;
|
||||
}
|
||||
|
||||
} else {
|
||||
PX4_ERR("alloc failed");
|
||||
}
|
||||
|
||||
delete instance;
|
||||
_object.store(nullptr);
|
||||
_task_id = -1;
|
||||
|
||||
return PX4_ERROR;
|
||||
}
|
||||
|
||||
int SensorAirspeedSim::custom_command(int argc, char *argv[])
|
||||
{
|
||||
return print_usage("unknown command");
|
||||
}
|
||||
|
||||
int SensorAirspeedSim::print_usage(const char *reason)
|
||||
{
|
||||
if (reason) {
|
||||
PX4_WARN("%s\n", reason);
|
||||
}
|
||||
|
||||
PRINT_MODULE_DESCRIPTION(
|
||||
R"DESCR_STR(
|
||||
### Description
|
||||
|
||||
|
||||
)DESCR_STR");
|
||||
|
||||
PRINT_MODULE_USAGE_NAME("sensor_arispeed_sim", "system");
|
||||
PRINT_MODULE_USAGE_COMMAND("start");
|
||||
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
|
||||
|
||||
return 0;
|
||||
}
|
||||
|
||||
extern "C" __EXPORT int sensor_airspeed_sim_main(int argc, char *argv[])
|
||||
{
|
||||
return SensorAirspeedSim::main(argc, argv);
|
||||
}
|
||||
@@ -0,0 +1,95 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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
|
||||
|
||||
#include <lib/perf/perf_counter.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>
|
||||
#include <uORB/PublicationMulti.hpp>
|
||||
#include <uORB/Subscription.hpp>
|
||||
#include <uORB/SubscriptionInterval.hpp>
|
||||
#include <uORB/topics/parameter_update.h>
|
||||
#include <uORB/topics/differential_pressure.h>
|
||||
#include <uORB/topics/vehicle_attitude.h>
|
||||
#include <uORB/topics/vehicle_global_position.h>
|
||||
#include <uORB/topics/vehicle_local_position.h>
|
||||
|
||||
using namespace time_literals;
|
||||
|
||||
static constexpr float TEMPERATURE_MSL = 288.15; // temperature at MSL [K] (15 [C])
|
||||
static constexpr float PRESSURE_MSL = 101325.0; // pressure at MSL [Pa]
|
||||
static constexpr float LAPSE_RATE = 0.0065; // reduction in temperature with altitude for troposphere [K/m]
|
||||
static constexpr float AIR_DENSITY_MSL = 1.225; // air density at MSL [kg/m^3]
|
||||
|
||||
class SensorAirspeedSim : public ModuleBase<SensorAirspeedSim>, public ModuleParams, public px4::ScheduledWorkItem
|
||||
{
|
||||
public:
|
||||
SensorAirspeedSim();
|
||||
~SensorAirspeedSim() override;
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int task_spawn(int argc, char *argv[]);
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int custom_command(int argc, char *argv[]);
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int print_usage(const char *reason = nullptr);
|
||||
|
||||
bool init();
|
||||
|
||||
private:
|
||||
void Run() override;
|
||||
|
||||
// generate white Gaussian noise sample with std=1
|
||||
static float generate_wgn();
|
||||
|
||||
// generate white Gaussian noise sample as a 3D vector with specified std
|
||||
matrix::Vector3f noiseGauss3f(float stdx, float stdy, float stdz) { return matrix::Vector3f(generate_wgn() * stdx, generate_wgn() * stdy, generate_wgn() * stdz); }
|
||||
|
||||
uORB::SubscriptionInterval _parameter_update_sub{ORB_ID(parameter_update), 1_s};
|
||||
uORB::Subscription _vehicle_attitude_sub{ORB_ID(vehicle_attitude)};
|
||||
uORB::Subscription _vehicle_global_position_sub{ORB_ID(vehicle_global_position_groundtruth)};
|
||||
uORB::Subscription _vehicle_local_position_sub{ORB_ID(vehicle_local_position_groundtruth)};
|
||||
|
||||
uORB::PublicationMulti<differential_pressure_s> _differential_pressure_pub{ORB_ID(differential_pressure)};
|
||||
|
||||
perf_counter_t _loop_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": cycle")};
|
||||
|
||||
// DEFINE_PARAMETERS(
|
||||
// (ParamInt<px4::params::SIM_GPS_USED>) _sim_gps_used
|
||||
// )
|
||||
};
|
||||
@@ -0,0 +1,41 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* simulated GPS number of satellites used
|
||||
*
|
||||
* @min 0
|
||||
* @max 50
|
||||
* @group Simulator
|
||||
*/
|
||||
// PARAM_DEFINE_INT32(SIM_GPS_USED, 10);
|
||||
Reference in New Issue
Block a user