Rover module: Temp

also add dependency on control allocation parameter CA_R_REV

.ci/Jenkinsfile-compile

@@ -88,7 +88,6 @@ pipeline {
                      "nxp_fmuk66-e_socketcan",
                      "nxp_fmuk66-v3_default",
                      "nxp_fmuk66-v3_socketcan",
-                     "nxp_fmurt1062-v1_default",
                      "nxp_mr-canhubk3_default",
                      "nxp_ucans32k146_canbootloader",
                      "nxp_ucans32k146_default",
@@ -111,6 +110,8 @@ pipeline {
                      "px4_fmu-v6c_default",
                      "px4_fmu-v6u_default",
                      "px4_fmu-v6x_default",
+                     "px4_fmu-v6xrt_bootloader",
+                     "px4_fmu-v6xrt_default",
                      "px4_io-v2_default",
                      "raspberrypi_pico_default",
                      "sky-drones_smartap-airlink_default",

.github/workflows/compile_macos.yml

@@ -18,6 +18,11 @@ jobs:
           px4_sitl
           ]
     steps:
+    - name: install Python 3.10
+      uses: actions/setup-python@v4
+      with:
+        python-version: "3.10"
+
     - uses: actions/checkout@v1
       with:
         token: ${{secrets.ACCESS_TOKEN}}

.github/workflows/compile_nuttx.yml

@@ -57,7 +57,6 @@ jobs:
           mro_x21-777,
           nxp_fmuk66-e,
           nxp_fmuk66-v3,
-          nxp_fmurt1062-v1,
           nxp_mr-canhubk3,
           nxp_ucans32k146,
           omnibus_f4sd,
@@ -70,6 +69,7 @@ jobs:
           px4_fmu-v6c,
           px4_fmu-v6u,
           px4_fmu-v6x,
+          px4_fmu-v6xrt,
           raspberrypi_pico,
           sky-drones_smartap-airlink,
           spracing_h7extreme,

.github/workflows/metadata.yml

@@ -128,4 +128,6 @@ jobs:
       run: |
         git clone https://github.com/PX4/px4_msgs.git
         rm px4_msgs/msg/*.msg
+        rm px4_msgs/srv/*.srv
         cp msg/*.msg px4_msgs/msg/
+        cp srv/*.srv px4_msgs/srv/

.github/workflows/nuttx_env_config.yml

@@ -0,0 +1,32 @@
+name: Nuttx Target with extra env config
+
+on:
+  push:
+    branches:
+    - 'main'
+  pull_request:
+    branches:
+    - '*'
+
+jobs:
+  build:
+    runs-on: ubuntu-latest
+    container: px4io/px4-dev-nuttx-focal:2022-08-12
+    strategy:
+      matrix:
+        config: [
+          px4_fmu-v5,
+          ]
+    steps:
+    - uses: actions/checkout@v1
+      with:
+        token: ${{secrets.ACCESS_TOKEN}}
+
+    - name: make ${{matrix.config}}
+      env:
+        PX4_EXTRA_NUTTX_CONFIG: "CONFIG_NSH_LOGIN_PASSWORD=\"test\";CONFIG_NSH_CONSOLE_LOGIN=y"
+      run: |
+        echo "PX4_EXTRA_NUTTX_CONFIG: $PX4_EXTRA_NUTTX_CONFIG"
+        make ${{matrix.config}} nuttx_context
+        # Check that the config option is set
+        grep CONFIG_NSH_LOGIN_PASSWORD build/${{matrix.config}}_default/NuttX/nuttx/.config

.gitmodules

@@ -75,3 +75,7 @@
 [submodule "src/lib/heatshrink/heatshrink"]
 	path = src/lib/heatshrink/heatshrink
 	url = https://github.com/PX4/heatshrink.git
+	branch = px4
+[submodule "Tools/simulation/gz"]
+	path = Tools/simulation/gz
+	url = https://github.com/PX4/PX4-gazebo-models.git

.vscode/cmake-variants.yaml

@@ -81,6 +81,16 @@ CONFIG:
       buildType: MinSizeRel
       settings:
         CONFIG: px4_fmu-v6x_bootloader
+    px4_fmu-v6xrt_default:
+      short: px4_fmu-v6xrt
+      buildType: MinSizeRel
+      settings:
+        CONFIG: px4_fmu-v6xrt_default
+    px4_fmu-v6xrt_bootloader:
+      short: px4_fmu-v6xrt_bootloader
+      buildType: MinSizeRel
+      settings:
+        CONFIG: px4_fmu-v6xrt_bootloader
     airmind_mindpx-v2_default:
       short: airmind_mindpx-v2
       buildType: MinSizeRel
@@ -181,6 +191,11 @@ CONFIG:
       buildType: MinSizeRel
       settings:
         CONFIG: cubepilot_cubeorange_test
+    cubepilot_cubeorangeplus_test:
+      short: cubepilot_cubeorangeplus
+      buildType: MinSizeRel
+      settings:
+        CONFIG: cubepilot_cubeorangeplus_test
     emlid_navio2_default:
       short: emlid_navio2
       buildType: MinSizeRel

CMakeLists.txt

@@ -148,6 +148,7 @@ define_property(GLOBAL PROPERTY PX4_MODULE_PATHS
                  BRIEF_DOCS "PX4 module paths"
                  FULL_DOCS "List of paths to all PX4 modules"
                  )
+
 define_property(GLOBAL PROPERTY PX4_SRC_FILES
                  BRIEF_DOCS "src files from all PX4 modules & libs"
                  FULL_DOCS "SRC files from px4_add_{module,library}"

Jenkinsfile

@@ -105,6 +105,7 @@ pipeline {
             ./emsdk activate latest;
             cd ..;
             . ./_emscripten_sdk/emsdk_env.sh;
+            git fetch --all --tags;
             make failsafe_web;
             cd build/px4_sitl_default_failsafe_web;
             mkdir -p failsafe_sim;
@@ -230,7 +231,9 @@ pipeline {
               sh("git clone https://${GIT_USER}:${GIT_PASS}@github.com/PX4/px4_msgs.git")
               // 'main' branch
               sh('rm -f px4_msgs/msg/*.msg')
+              sh('rm -f px4_msgs/srv/*.srv')
               sh('cp msg/*.msg px4_msgs/msg/')
+              sh('cp srv/*.srv px4_msgs/srv/')
               sh('cd px4_msgs; git status; git add .; git commit -a -m "Update message definitions `date`" || true')
               sh('cd px4_msgs; git push origin main || true')
               sh('rm -rf px4_msgs')

Makefile

@@ -266,7 +266,6 @@ px4fmu_firmware: \
 
 misc_qgc_extra_firmware: \
 	check_nxp_fmuk66-v3_default \
-	check_nxp_fmurt1062-v1_default \
 	check_mro_x21_default \
 	check_bitcraze_crazyflie_default \
 	check_bitcraze_crazyflie21_default \

ROMFS/px4fmu_common/init.d-posix/airframes/1040_gazebo-classic_standard_vtol

@@ -47,6 +47,8 @@ param set-default PWM_MAIN_FUNC6 201
 param set-default PWM_MAIN_FUNC7 202
 param set-default PWM_MAIN_FUNC8 203
 
+param set-default FW_AIRSPD_MAX 25
+param set-default FW_THR_ASPD_MAX 0.4
 param set-default NPFG_PERIOD 12
 param set-default FW_PR_FF 0.2
 param set-default FW_PR_P 0.9
@@ -62,19 +64,18 @@ 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_ROLL_P 4
 param set-default MC_ROLLRATE_P 0.3
 param set-default MC_YAW_P 1.6
+param set-default MC_YAWRATE_P 0.3
+
 
 param set-default MIS_TAKEOFF_ALT 10
 
-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_FWD_THRUST_SC 1
 param set-default VT_F_TRANS_THR 0.75
 param set-default VT_TYPE 2
 

ROMFS/px4fmu_common/init.d-posix/airframes/1061_gazebo-classic_r1_rover

@@ -4,31 +4,9 @@
 # @type Rover
 # @class Rover
 
-. ${R}etc/init.d/rc.rover_defaults
+. ${R}etc/init.d/rc.rover_differential_defaults
 
-param set-default GND_L1_DIST 5
-param set-default GND_SP_CTRL_MODE 1
-param set-default GND_SPEED_D 3
-param set-default GND_SPEED_I 0.001
-param set-default GND_SPEED_IMAX 0.125
-param set-default GND_SPEED_P 0.25
-param set-default GND_SPEED_THR_SC 1
-param set-default GND_SPEED_TRIM 4
-param set-default GND_THR_CRUISE 0.3
-param set-default GND_THR_MAX 0.5
-param set-default GND_THR_MIN 0
-
-param set-default NAV_ACC_RAD 0.5
-param set-default NAV_LOITER_RAD 2
-
-param set-default GND_MAX_ANG 0.6
-param set-default GND_WHEEL_BASE 2.0
-
-param set-default CA_AIRFRAME 6
-
-param set-default CA_R_REV 3
 param set-default PWM_MAIN_FUNC1 101
 param set-default PWM_MAIN_FUNC2 101
 param set-default PWM_MAIN_FUNC6 102
 param set-default PWM_MAIN_FUNC7 102
-

ROMFS/px4fmu_common/init.d-posix/airframes/4004_gz_standard_vtol

@@ -76,7 +76,7 @@ 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 NPFG_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

ROMFS/px4fmu_common/init.d-posix/airframes/4006_gz_px4vision

@@ -52,12 +52,8 @@ param set-default MAV_1_MODE 9
 # param set-default SER_TEL1_BAUD 921600	Not found
 
 # Vehicle attitude PID tuning
-param set-default MC_ACRO_EXPO 0
-param set-default MC_ACRO_EXPO_Y 0
 param set-default MC_ACRO_P_MAX 200
 param set-default MC_ACRO_R_MAX 200
-param set-default MC_ACRO_SUPEXPO 0
-param set-default MC_ACRO_SUPEXPOY 0
 param set-default MC_ACRO_Y_MAX 150
 param set-default MC_PITCHRATE_D 0.0015
 param set-default MC_ROLLRATE_D 0.0015

ROMFS/px4fmu_common/init.d-posix/airframes/4009_gz_r1_rover

@@ -0,0 +1,31 @@
+#!/bin/sh
+# @name Aion Robotics R1 Rover
+# @type Rover
+# @class Rover
+
+. ${R}etc/init.d/rc.rover_differential_defaults
+
+PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
+PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
+PX4_SIM_MODEL=${PX4_SIM_MODEL:=r1_rover}
+
+param set-default SIM_GZ_EN 1 # Gazebo bridge
+
+# Simulated sensors
+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
+
+# Actuator mapping
+param set-default SIM_GZ_WH_FUNC1 101 # right wheel
+param set-default SIM_GZ_WH_MIN1 0
+param set-default SIM_GZ_WH_MAX1 200
+param set-default SIM_GZ_WH_DIS1 100
+
+param set-default SIM_GZ_WH_FUNC2 102 # left wheel
+param set-default SIM_GZ_WH_MIN2 0
+param set-default SIM_GZ_WH_MAX2 200
+param set-default SIM_GZ_WH_DIS2 100
+
+param set-default SIM_GZ_WH_REV 1 # reverse right wheel

ROMFS/px4fmu_common/init.d-posix/airframes/4010_gz_x500_mono_cam

@@ -0,0 +1,10 @@
+#!/bin/sh
+#
+# @name Gazebo x500 mono cam
+#
+# @type Quadrotor
+#
+
+PX4_SIM_MODEL=${PX4_SIM_MODEL:=x500_mono_cam}
+
+. ${R}etc/init.d-posix/airframes/4001_gz_x500

ROMFS/px4fmu_common/init.d-posix/airframes/CMakeLists.txt

@@ -80,6 +80,8 @@ px4_add_romfs_files(
 	4005_gz_x500_vision
 	4006_gz_px4vision
 	4008_gz_advanced_plane
+	4009_gz_r1_rover
+	4010_gz_x500_mono_cam
 
 	6011_gazebo-classic_typhoon_h480
 	6011_gazebo-classic_typhoon_h480.post

ROMFS/px4fmu_common/init.d-posix/px4-rc.simulator

@@ -36,8 +36,10 @@ if [ "$PX4_SIMULATOR" = "sihsim" ] || [ "$(param show -q SYS_AUTOSTART)" -eq "0"
 		exit 1
 	fi
 
-elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; then
+elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" = "1" ]; then
+	# Use Gazebo
 
+	echo "INFO  [init] Gazebo simulator"
 
 	# set local coordinate frame reference
 	if [ -n "${PX4_HOME_LAT}" ]; then
@@ -49,21 +51,13 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
 	fi
 
 	if [ -n "${PX4_HOME_ALT}" ]; then
-		param set SIM_GZ_HOME_ALT ${PX4_HOME_LON}
+		param set SIM_GZ_HOME_ALT ${PX4_HOME_ALT}
 	fi
 
-	# source generated gz_env.sh for GZ_SIM_RESOURCE_PATH
-	if [ -f ./gz_env.sh ]; then
-		. ./gz_env.sh
+	# Only start up Gazebo if PX4_GZ_STANDALONE is not set.
+	if [ -z "${PX4_GZ_STANDALONE}" ]; then
 
-	elif [ -f ../gz_env.sh ]; then
-		. ../gz_env.sh
-	fi
-
-	# Only start up Gazebo if STANDALONE set to false
-	if [ "$STANDALONE" != '1' ]; then
-
-		# "gz sim" only avaiilable in Garden and later
+		# "gz sim" only available in Garden and later
 		GZ_SIM_VERSIONS=$(gz sim --versions 2>&1)
 		if [ $? -eq 0 ] && [ "${GZ_SIM_VERSIONS}" != "" ]
 		then
@@ -79,7 +73,15 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
 		gz_world=$( ${gz_command} topic -l | grep -m 1 -e "^/world/.*/clock" | sed 's/\/world\///g; s/\/clock//g' )
 
 		# shellcheck disable=SC2153
-		if [ -z "${gz_world}" ] && [ -n "${PX4_GZ_WORLDS}" ] && [ -n "${PX4_GZ_WORLD}" ]; then
+		if [ -z "${gz_world}" ] && [ -n "${PX4_GZ_WORLD}" ]; then
+
+			# source generated gz_env.sh for GZ_SIM_RESOURCE_PATH
+			if [ -f ./gz_env.sh ]; then
+				. ./gz_env.sh
+
+			elif [ -f ../gz_env.sh ]; then
+				. ../gz_env.sh
+			fi
 
 			echo "INFO  [init] starting gazebo with world: ${PX4_GZ_WORLDS}/${PX4_GZ_WORLD}.sdf"
 
@@ -91,107 +93,70 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" -eq "1" ]; th
 			fi
 
 		else
+			# Gazebo is already running, do not start the simulator, nor the GUI
 			echo "INFO  [init] gazebo already running world: ${gz_world}"
 			PX4_GZ_WORLD=${gz_world}
 		fi
+	else
+		echo "INFO  [init] Standalone PX4 launch, waiting for Gazebo"
 	fi
 
 	# start gz_bridge
-	if [ -n "${PX4_GZ_MODEL}" ] && [ -z "${PX4_GZ_MODEL_NAME}" ]; then
+	if [ -n "${PX4_SIM_MODEL#*gz_}" ] && [ -z "${PX4_GZ_MODEL_NAME}" ]; then
 		# model specified, gz_bridge will spawn model
 
 		if [ -n "${PX4_GZ_MODEL_POSE}" ]; then
+			# model pose provided: [x, y, z, roll, pitch, yaw]
+
 			# Clean potential input line formatting.
 			model_pose="$( echo "${PX4_GZ_MODEL_POSE}" | sed -e 's/^[ \t]*//; s/[ \t]*$//; s/,/ /g; s/  / /g; s/ /,/g' )"
 			echo "INFO  [init] PX4_GZ_MODEL_POSE set, spawning at: ${model_pose}"
 
 		else
+			# model pose not provided, origin will be used
+
 			echo "WARN  [init] PX4_GZ_MODEL_POSE not set, spawning at origin."
 			model_pose="0,0,0,0,0,0"
 		fi
 
 		# start gz bridge with pose arg.
-		if gz_bridge start -p "${model_pose}" -m "${PX4_GZ_MODEL}" -w "${PX4_GZ_WORLD}" -i "${px4_instance}"; then
-			if param compare -s SENS_EN_BAROSIM 1
-			then
-				sensor_baro_sim start
-			fi
-			if param compare -s SENS_EN_GPSSIM 1
-			then
-				sensor_gps_sim start
-			fi
-			if param compare -s SENS_EN_MAGSIM 1
-			then
-				sensor_mag_sim start
-			fi
-			if param compare -s SENS_EN_ARSPDSIM 1
-			then
-				sensor_airspeed_sim start
-			fi
-
-		else
-			echo "ERROR [init] gz_bridge failed to start"
+		if ! gz_bridge start -p "${model_pose}" -m "${PX4_SIM_MODEL#*gz_}" -w "${PX4_GZ_WORLD}" -i "${px4_instance}"; then
+			echo "ERROR [init] gz_bridge failed to start and spawn model"
 			exit 1
 		fi
 
-	elif [ -n "${PX4_GZ_MODEL_NAME}" ] && [ -z "${PX4_GZ_MODEL}" ]; then
+	elif [ -n "${PX4_GZ_MODEL_NAME}" ]; then
 		# model name specificed, gz_bridge will attach to existing model
 
-		if gz_bridge start -n "${PX4_GZ_MODEL_NAME}" -w "${PX4_GZ_WORLD}"; then
-			if param compare -s SENS_EN_BAROSIM 1
-			then
-				sensor_baro_sim start
-			fi
-			if param compare -s SENS_EN_GPSSIM 1
-			then
-				sensor_gps_sim start
-			fi
-			if param compare -s SENS_EN_MAGSIM 1
-			then
-				sensor_mag_sim start
-			fi
-			if param compare -s SENS_EN_ARSPDSIM 1
-			then
-				sensor_airspeed_sim start
-			fi
-
-		else
-			echo "ERROR [init] gz_bridge failed to start"
-			exit 1
-		fi
-
-	elif [ -n "${PX4_SIM_MODEL}" ] && [ -z "${PX4_GZ_MODEL_NAME}" ] && [ -z "${PX4_GZ_MODEL}" ]; then
-
-		echo "WARN  [init] PX4_GZ_MODEL_NAME or PX4_GZ_MODEL not set using PX4_SIM_MODEL."
-
-		if gz_bridge start -m "${PX4_SIM_MODEL#*gz_}" -w "${PX4_GZ_WORLD}" -i "${px4_instance}"; then
-			if param compare -s SENS_EN_BAROSIM 1
-			then
-				sensor_baro_sim start
-			fi
-			if param compare -s SENS_EN_GPSSIM 1
-			then
-				sensor_gps_sim start
-			fi
-			if param compare -s SENS_EN_MAGSIM 1
-			then
-				sensor_mag_sim start
-			fi
-			if param compare -s SENS_EN_ARSPDSIM 1
-			then
-				sensor_airspeed_sim start
-			fi
-
-		else
-			echo "ERROR [init] gz_bridge failed to start"
+		echo "INFO  [init] PX4_GZ_MODEL_NAME set, PX4 will attach to existing model"
+		if ! gz_bridge start -n "${PX4_GZ_MODEL_NAME}" -w "${PX4_GZ_WORLD}"; then
+			echo "ERROR [init] gz_bridge failed to start and attach to existing model"
 			exit 1
 		fi
 
 	else
-		echo "ERROR [init] failed to pass only PX4_GZ_MODEL_NAME or PX4_GZ_MODEL"
+		echo "ERROR [init] failed to pass only PX4_GZ_MODEL_NAME or PX4_SIM_MODEL"
 		exit 1
 	fi
 
+	# Start the sensor simulator modules
+	if param compare -s SENS_EN_BAROSIM 1
+	then
+		sensor_baro_sim start
+	fi
+	if param compare -s SENS_EN_GPSSIM 1
+	then
+		sensor_gps_sim start
+	fi
+	if param compare -s SENS_EN_MAGSIM 1
+	then
+		sensor_mag_sim start
+	fi
+	if param compare -s SENS_EN_ARSPDSIM 1
+	then
+		sensor_airspeed_sim start
+	fi
+
 elif [ "$PX4_SIM_MODEL" = "jmavsim_iris" ] || [ "$(param show -q SYS_AUTOSTART)" -eq "10017" ]; then
 
 	echo "INFO  [init] jMAVSim simulator"

ROMFS/px4fmu_common/init.d/CMakeLists.txt

@@ -51,6 +51,8 @@ px4_add_romfs_files(
 	rc.thermal_cal
 	rc.rover_apps
 	rc.rover_defaults
+	rc.rover_differential_apps
+	rc.rover_differential_defaults
 	rc.uuv_apps
 	rc.uuv_defaults
 	rc.vehicle_setup

ROMFS/px4fmu_common/init.d/airframes/4016_holybro_px4vision

@@ -45,12 +45,8 @@ param set-default MAV_1_MODE 9
 param set-default SER_TEL1_BAUD 921600
 
 # Vehicle attitude PID tuning
-param set-default MC_ACRO_EXPO 0
-param set-default MC_ACRO_EXPO_Y 0
 param set-default MC_ACRO_P_MAX 200
 param set-default MC_ACRO_R_MAX 200
-param set-default MC_ACRO_SUPEXPO 0
-param set-default MC_ACRO_SUPEXPOY 0
 param set-default MC_ACRO_Y_MAX 150
 param set-default MC_PITCHRATE_D 0.0015
 param set-default MC_ROLLRATE_D 0.0015

ROMFS/px4fmu_common/init.d/airframes/4020_holybro_px4vision_v1_5

@@ -45,12 +45,8 @@ param set-default MAV_1_MODE 9
 param set-default SER_TEL1_BAUD 921600
 
 # Vehicle attitude PID tuning
-param set-default MC_ACRO_EXPO 0
-param set-default MC_ACRO_EXPO_Y 0
 param set-default MC_ACRO_P_MAX 200
 param set-default MC_ACRO_R_MAX 200
-param set-default MC_ACRO_SUPEXPO 0
-param set-default MC_ACRO_SUPEXPOY 0
 param set-default MC_ACRO_Y_MAX 150
 param set-default MC_PITCHRATE_D 0.0015
 param set-default MC_ROLLRATE_D 0.0015

ROMFS/px4fmu_common/init.d/airframes/4040_reaper

@@ -1,65 +0,0 @@
-#!/bin/sh
-#
-# @name Reaper 500 Quad
-#
-# @type Quadrotor H
-# @class Copter
-#
-# @maintainer Blankered
-#
-# @board px4_fmu-v2 exclude
-# @board bitcraze_crazyflie exclude
-#
-
-. ${R}etc/init.d/rc.mc_defaults
-
-param set-default MC_ROLLRATE_P 0.14
-param set-default MC_ROLLRATE_I 0.1
-param set-default MC_ROLLRATE_D 0.004
-param set-default MC_PITCH_P 6
-param set-default MC_PITCHRATE_P 0.14
-param set-default MC_PITCHRATE_I 0.09
-param set-default MC_PITCHRATE_D 0.004
-param set-default MC_YAW_P 4
-
-param set-default NAV_ACC_RAD 2
-
-param set-default RTL_RETURN_ALT 30
-param set-default RTL_DESCEND_ALT 10
-
-param set-default CA_ROTOR_COUNT 4
-param set-default CA_ROTOR0_PX 0.15
-param set-default CA_ROTOR0_PY 0.15
-param set-default CA_ROTOR0_KM -0.05
-param set-default CA_ROTOR1_PX -0.15
-param set-default CA_ROTOR1_PY -0.15
-param set-default CA_ROTOR1_KM -0.05
-param set-default CA_ROTOR2_PX 0.15
-param set-default CA_ROTOR2_PY -0.15
-param set-default CA_ROTOR2_KM 0.05
-param set-default CA_ROTOR3_PX -0.15
-param set-default CA_ROTOR3_PY 0.15
-param set-default CA_ROTOR3_KM 0.05
-
-param set-default PWM_MAIN_FUNC1 101
-param set-default PWM_MAIN_FUNC2 102
-param set-default PWM_MAIN_FUNC3 103
-param set-default PWM_MAIN_FUNC4 104
-param set-default PWM_MAIN_MIN1 1100
-param set-default PWM_MAIN_MIN2 1100
-param set-default PWM_MAIN_MIN3 1100
-param set-default PWM_MAIN_MIN4 1100
-param set-default PWM_MAIN_MAX1 1900
-param set-default PWM_MAIN_MAX2 1900
-param set-default PWM_MAIN_MAX3 1900
-param set-default PWM_MAIN_MAX4 1900
-
-param set-default PWM_MAIN_TIM0 50
-param set-default PWM_MAIN_TIM1 50
-param set-default PWM_MAIN_TIM2 50
-
-param set-default PWM_AUX_TIM0 50
-param set-default PWM_AUX_TIM1 50
-param set-default PWM_AUX_TIM2 50
-
-

ROMFS/px4fmu_common/init.d/airframes/4900_crazyflie

@@ -1,91 +0,0 @@
-#!/bin/sh
-#
-# @name Crazyflie 2
-#
-# @type Quadrotor x
-# @class Copter
-#
-# @maintainer Dennis Shtatov <densht@gmail.com>
-#
-# @board px4_fmu-v2 exclude
-# @board px4_fmu-v3 exclude
-# @board px4_fmu-v4 exclude
-# @board px4_fmu-v4pro exclude
-# @board px4_fmu-v5 exclude
-# @board px4_fmu-v5x exclude
-# @board diatone_mamba-f405-mk2 exclude
-#
-. ${R}etc/init.d/rc.mc_defaults
-
-param set-default BAT1_N_CELLS 1
-param set-default BAT1_CAPACITY 240
-param set-default BAT1_SOURCE 1
-
-param set-default CBRK_SUPPLY_CHK 894281
-param set-default COM_RC_IN_MODE 1
-
-param set-default EKF2_ABL_LIM 2
-param set-default EKF2_HGT_REF 2
-param set-default EKF2_RNG_CTRL 2
-param set-default EKF2_MAG_TYPE 1
-param set-default EKF2_OF_CTRL 1
-param set-default EKF2_OF_DELAY 10
-
-param set-default IMU_GYRO_CUTOFF 100
-param set-default IMU_ACCEL_CUTOFF 30
-
-param set-default MC_AIRMODE 1
-param set-default IMU_DGYRO_CUTOFF 70
-param set-default MC_PITCHRATE_D 0.002
-param set-default MC_PITCHRATE_P 0.07
-param set-default MC_ROLLRATE_D 0.002
-param set-default MC_ROLLRATE_P 0.07
-param set-default MC_YAW_P 3
-
-param set-default MPC_THR_HOVER 0.7
-param set-default MPC_Z_P 1.5
-param set-default MPC_Z_VEL_P_ACC 8
-param set-default MPC_Z_VEL_I_ACC 6
-param set-default MPC_HOLD_MAX_XY 0.1
-param set-default MPC_MAX_FLOW_HGT 3
-
-param set-default NAV_RCL_ACT 3
-
-param set-default CA_ROTOR_COUNT 4
-param set-default CA_ROTOR0_PX 0.03
-param set-default CA_ROTOR0_PY 0.03
-param set-default CA_ROTOR1_PX -0.03
-param set-default CA_ROTOR1_PY 0.03
-param set-default CA_ROTOR1_KM -0.05
-param set-default CA_ROTOR2_PX -0.03
-param set-default CA_ROTOR2_PY -0.03
-param set-default CA_ROTOR3_PX 0.03
-param set-default CA_ROTOR3_PY -0.03
-param set-default CA_ROTOR3_KM -0.05
-
-# Run the motors at 328.125 kHz (recommended)
-param set-default PWM_MAIN_TIM0 3921
-param set-default PWM_MAIN_TIM1 3921
-
-param set-default PWM_MAIN_FUNC1 101
-param set-default PWM_MAIN_FUNC2 102
-param set-default PWM_MAIN_FUNC3 103
-param set-default PWM_MAIN_FUNC4 104
-param set-default PWM_MAIN_DIS0 0
-param set-default PWM_MAIN_DIS1 0
-param set-default PWM_MAIN_DIS2 0
-param set-default PWM_MAIN_DIS3 0
-param set-default PWM_MAIN_MIN0 0
-param set-default PWM_MAIN_MIN1 0
-param set-default PWM_MAIN_MIN2 0
-param set-default PWM_MAIN_MIN3 0
-param set-default PWM_MAIN_MAX0 255
-param set-default PWM_MAIN_MAX1 255
-param set-default PWM_MAIN_MAX2 255
-param set-default PWM_MAIN_MAX3 255
-
-
-param set-default SENS_FLOW_MINRNG 0.05
-
-syslink start
-mavlink start -d /dev/bridge0 -b 57600 -m osd -r 40000

ROMFS/px4fmu_common/init.d/airframes/50003_aion_robotics_r1_rover

@@ -11,51 +11,15 @@
 # @board bitcraze_crazyflie exclude
 #
 
-. ${R}etc/init.d/rc.rover_defaults
+. ${R}etc/init.d/rc.rover_differential_defaults
 
 param set-default BAT1_N_CELLS 4
 
 param set-default EKF2_GBIAS_INIT 0.01
 param set-default EKF2_ANGERR_INIT 0.01
-param set-default EKF2_MAG_TYPE 1
-
-param set-default FW_AIRSPD_MIN 0
-param set-default FW_AIRSPD_TRIM 1
-param set-default FW_AIRSPD_MAX 3
-
-param set-default GND_SP_CTRL_MODE 1
-param set-default GND_L1_DIST 5
-param set-default GND_L1_PERIOD 3
-param set-default GND_THR_CRUISE 0.7
-param set-default GND_THR_MAX 0.5
-
-# Because this is differential drive, it can make a turn with radius 0.
-# This corresponds to a turn angle of pi radians.
-# If a special case is made for differential-drive, this will need to change.
-param set-default GND_MAX_ANG 3.142
-param set-default GND_WHEEL_BASE 0.3
-
-# TODO: Set to -1.0, to allow reversing. This will require many changes in the codebase
-# to support negative throttle.
-param set-default GND_THR_MIN 0
-param set-default GND_SPEED_P 0.25
-param set-default GND_SPEED_I 3
-param set-default GND_SPEED_D 0.001
-param set-default GND_SPEED_IMAX 0.125
-param set-default GND_SPEED_THR_SC 1
-
-param set-default NAV_ACC_RAD 0.5
-
-# Differential drive acts like ackermann steering with a maximum turn angle of 180 degrees, or pi radians
-param set-default GND_MAX_ANG 3.1415
 
 # Set geometry & output configration
-param set-default CA_AIRFRAME 6
-param set-default CA_R_REV 3
-param set-default PWM_MAIN_FUNC1 101
-param set-default PWM_MAIN_FUNC2 102
-param set-default PWM_MAIN_DIS1 1500
-param set-default PWM_MAIN_DIS2 1500
-param set-default PWM_MAIN_TIM0 50
-param set-default PWM_MAIN_TIM1 50
-
+param set-default RBCLW_ADDRESS 128
+param set-default RBCLW_FUNC1 101
+param set-default RBCLW_FUNC2 102
+param set-default RBCLW_REV 1 # reverse right wheels

ROMFS/px4fmu_common/init.d/airframes/CMakeLists.txt

@@ -58,7 +58,6 @@ px4_add_romfs_files(
 	4017_nxp_hovergames
 	4019_x500_v2
 	4020_holybro_px4vision_v1_5
-	4040_reaper
 	4041_beta75x
 	4050_generic_250
 	4052_holybro_qav250
@@ -67,7 +66,6 @@ px4_add_romfs_files(
 	4071_ifo
 	4073_ifo-s
 	4500_clover4
-	4900_crazyflie
 	4901_crazyflie21
 
 	# [5000, 5999] Quadrotor +"

ROMFS/px4fmu_common/init.d/rc.fw_defaults

@@ -17,7 +17,7 @@ param set-default COM_POS_FS_DELAY 5
 
 # there is a 2.5 factor applied on the _FS thresholds if for invalidation
 param set-default COM_POS_FS_EPH 50
-param set-default COM_VEL_FS_EVH 5
+param set-default COM_VEL_FS_EVH 3
 
 param set-default COM_POS_LOW_EPH 50
 

ROMFS/px4fmu_common/init.d/rc.rover_apps

@@ -9,8 +9,6 @@
 # Start the attitude and position estimator.
 #
 ekf2 start &
-#attitude_estimator_q start
-#local_position_estimator start
 
 #
 # Start Control Allocator
@@ -22,7 +20,6 @@ control_allocator start
 #
 rover_pos_control start
 
-
 #
 # Start Land Detector.
 #

ROMFS/px4fmu_common/init.d/rc.rover_differential_apps

@@ -0,0 +1,11 @@
+#!/bin/sh
+# Standard apps for a differential drive rover.
+
+# Start the attitude and position estimator.
+ekf2 start &
+
+# Start rover differential drive controller.
+rover_control start
+
+# Start Land Detector.
+land_detector start rover

ROMFS/px4fmu_common/init.d/rc.rover_differential_defaults

@@ -0,0 +1,11 @@
+#!/bin/sh
+# Differential rover parameters.
+
+set VEHICLE_TYPE rover_differential
+
+param set-default MAV_TYPE 10 # MAV_TYPE_GROUND_ROVER
+
+param set-default CA_AIRFRAME 6 # Rover (Differential)
+param set-default CA_R_REV 3 # Right and left motors reversible
+
+param set-default EKF2_MAG_TYPE 1 # make sure magnetometer is fused even when not flying

ROMFS/px4fmu_common/init.d/rc.vehicle_setup

@@ -32,6 +32,15 @@ then
 	. ${R}etc/init.d/rc.rover_apps
 fi
 
+#
+# Differential Rover setup.
+#
+if [ $VEHICLE_TYPE = rover_differential ]
+then
+	# Start differential drive rover apps.
+	. ${R}etc/init.d/rc.rover_differential_apps
+fi
+
 #
 # VTOL setup.
 #

ROMFS/px4fmu_common/init.d/rcS

@@ -170,7 +170,7 @@ else
 		param select-backup $PARAM_BACKUP_FILE
 	fi
 
-	if ver hwcmp PX4_FMU_V5X PX4_FMU_V6X ARK_FMU_V6X
+	if ver hwcmp PX4_FMU_V5X PX4_FMU_V6X ARK_FMU_V6X PX4_FMU_V6XRT
 	then
 		netman update -i eth0
 	fi
@@ -274,12 +274,9 @@ else
 		. $FCONFIG
 	fi
 
-	#
-	# Start IO for PWM output or RC input if enabled
-	#
-	if param compare -s SYS_USE_IO 1
+	if px4io supported
 	then
-		# Check if PX4IO present and update firmware if needed.
+	# Check if PX4IO present and update firmware if needed.
 		if [ -f $IOFW ]
 		then
 			if ! px4io checkcrc ${IOFW}
@@ -301,12 +298,12 @@ else
 					tune_control stop
 				fi
 			fi
-		fi
 
-		if ! px4io start
-		then
-			echo "PX4IO start failed"
-			set STARTUP_TUNE 2 # tune 2 = ERROR_TUNE
+			if ! px4io start
+			then
+				echo "PX4IO start failed"
+				set STARTUP_TUNE 2 # tune 2 = ERROR_TUNE
+			fi
 		fi
 	fi
 

Tools/ecl_ekf/plotting/pdf_report.py

@@ -43,6 +43,11 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
     except:
         raise PreconditionError('could not find estimator_states instance', multi_instance)
 
+    try:
+        estimator_sensor_bias = ulog.get_dataset('estimator_sensor_bias', multi_instance).data
+    except:
+        raise PreconditionError('could not find estimator_sensor_bias instance', multi_instance)
+
     try:
         estimator_innovations = ulog.get_dataset('estimator_innovations', multi_instance).data
         estimator_innovation_variances = ulog.get_dataset('estimator_innovation_variances', multi_instance).data
@@ -299,21 +304,21 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
         data_plot.save()
         data_plot.close()
 
-        # Plot the delta angle bias estimates
+        # Plot the gyro bias estimates
         data_plot = CheckFlagsPlot(
-            1e-6 * estimator_states['timestamp'], estimator_states,
-            [['states[10]'], ['states[11]'], ['states[12]']],
-            x_label='time (sec)', y_labels=['X (rad)', 'Y (rad)', 'Z (rad)'],
-            plot_title='Delta Angle Bias Estimates', annotate=False, pdf_handle=pdf_pages)
+            1e-6 * estimator_sensor_bias['timestamp'], estimator_sensor_bias,
+            [['gyro_bias[0]'], ['gyro_bias[1]'], ['gyro_bias[2]']],
+            x_label='time (sec)', y_labels=['X (rad/s)', 'Y (rad/s)', 'Z (rad/s)'],
+            plot_title='Gyro Bias Estimates', annotate=False, pdf_handle=pdf_pages)
         data_plot.save()
         data_plot.close()
 
-        # Plot the delta velocity bias estimates
+        # Plot the accel bias estimates
         data_plot = CheckFlagsPlot(
-            1e-6 * estimator_states['timestamp'], estimator_states,
-            [['states[13]'], ['states[14]'], ['states[15]']],
-            x_label='time (sec)', y_labels=['X (m/s)', 'Y (m/s)', 'Z (m/s)'],
-            plot_title='Delta Velocity Bias Estimates', annotate=False, pdf_handle=pdf_pages)
+            1e-6 * estimator_sensor_bias['timestamp'], estimator_sensor_bias,
+            [['accel_bias[0]'], ['accel_bias[1]'], ['accel_bias[2]']],
+            x_label='time (sec)', y_labels=['X (m/s^2)', 'Y (m/s^2)', 'Z (m/s^2)'],
+            plot_title='Accel Bias Estimates', annotate=False, pdf_handle=pdf_pages)
         data_plot.save()
         data_plot.close()
 

Tools/module_config/output_groups_from_timer_config.py

@@ -80,6 +80,8 @@ def get_timer_groups(timer_config_file, verbose=False):
             max_num_channels = 16 # Just add a fixed number of timers
             timers = [str(i) for i in range(max_num_channels)]
             dshot_support = {str(i): False for i in range(max_num_channels)}
+            for i in range(8): # First 8 channels support dshot
+                dshot_support[str(i)] = True
             break
 
         if timer:

Tools/msg/px_generate_uorb_compressed_fields.py

@@ -146,6 +146,7 @@ def write_fields_to_hpp_file(file_name: str, definitions: dict, window_length: i
                              format_list: [str]):
     max_tokenized_field_length, max_tokenized_field_length_msg = max(
         ((len(definitions[k]['fields']), k) for k in definitions), key=itemgetter(0))
+    max_untokenized_field_length = max(definitions[k]['fields_total_length'] for k in definitions)
     max_num_orb_ids = max(len(definitions[k]['orb_ids']) for k in definitions)
     max_num_orb_id_dependencies = max(len(definitions[k]['dependencies']) for k in definitions)
 
@@ -167,6 +168,7 @@ const uint8_t* orb_compressed_message_formats();
 unsigned orb_compressed_message_formats_size();
 
 static constexpr unsigned orb_tokenized_fields_max_length = {MAX_TOKENIZED_FIELD_LENGTH}; // {MAX_TOKENIZED_FIELD_LENGTH_MSG}
+static constexpr unsigned orb_untokenized_fields_max_length = {MAX_UNTOKENIZED_FIELD_LENGTH};
 static constexpr unsigned orb_compressed_max_num_orb_ids = {MAX_NUM_ORB_IDS};
 static constexpr unsigned orb_compressed_max_num_orb_id_dependencies = {MAX_NUM_ORB_ID_DEPENDENCIES};
 
@@ -179,6 +181,7 @@ static constexpr unsigned orb_compressed_heatshrink_lookahead_length = {LOOKAHEA
 '''
                           .replace('{MAX_TOKENIZED_FIELD_LENGTH}', str(max_tokenized_field_length))
                           .replace('{MAX_TOKENIZED_FIELD_LENGTH_MSG}', max_tokenized_field_length_msg)
+                          .replace('{MAX_UNTOKENIZED_FIELD_LENGTH}', str(max_untokenized_field_length))
                           .replace('{MAX_NUM_ORB_IDS}', str(max_num_orb_ids))
                           .replace('{MAX_NUM_ORB_ID_DEPENDENCIES}', str(max_num_orb_id_dependencies))
                           .replace('{WINDOW_LENGTH}', str(window_length))

Tools/msg/templates/ucdr/msg.h.em

@@ -124,7 +124,7 @@ static inline constexpr int ucdr_topic_size_@(topic)()
 	return @(struct_size);
 }
 
-bool ucdr_serialize_@(topic)(const void* data, ucdrBuffer& buf, int64_t time_offset = 0)
+static inline bool ucdr_serialize_@(topic)(const void* data, ucdrBuffer& buf, int64_t time_offset = 0)
 {
 	const @(uorb_struct)& topic = *static_cast<const @(uorb_struct)*>(data);
 @{
@@ -153,7 +153,7 @@ for field_type, field_name, field_size, padding in fields:
 	return true;
 }
 
-bool ucdr_deserialize_@(topic)(ucdrBuffer& buf, @(uorb_struct)& topic, int64_t time_offset = 0)
+static inline bool ucdr_deserialize_@(topic)(ucdrBuffer& buf, @(uorb_struct)& topic, int64_t time_offset = 0)
 {
 @{
 for field_type, field_name, field_size, padding in fields:

Tools/msg/templates/uorb/msg.json.em

@@ -42,6 +42,7 @@ for field in spec.parsed_fields():
 {
 @# join all msg files in one line e.g: "float[3] position;float[3] velocity;bool armed;"
 		"fields": @( json.dumps(bytearray(";".join(topic_fields)+";", 'utf-8').decode('unicode_escape')) ),
+		"fields_total_length": @(sum([len(convert_type(field.type))+1+len(field.name)+1 for field in sorted_fields])),
 		"orb_ids": @( json.dumps([ all_topics.index(topic) for topic in topics]) ),
 		"main_orb_id": @( all_topics.index(name_snake_case) if name_snake_case in all_topics else -1 ),
 		"dependencies": @( json.dumps(list(set(dependencies))) ),

Tools/px_process_events.py

@@ -55,6 +55,10 @@ def main():
                         metavar="PATH",
                         nargs='*',
                         help="one or more paths/files to source files to scan for events")
+    parser.add_argument("-b", "--base-path",
+                        default="",
+                        metavar="PATH",
+                        help="path prefix for everything passed with --src-path")
     parser.add_argument("-j", "--json",
                         nargs='?',
                         const="events.json",
@@ -84,7 +88,7 @@ def main():
     # canonicalize + remove duplicates
     src_paths = set()
     for path in args.src_path:
-        src_paths.add(os.path.realpath(path))
+        src_paths.add(os.path.realpath(os.path.join(args.base_path, path)))
 
     if not scanner.ScanDir(src_paths, parser):
         sys.exit(1)

Tools/setup/arch.sh

@@ -1,7 +1,7 @@
 #! /usr/bin/env bash
 
 ## Bash script to setup PX4 development environment on Arch Linux.
-## Tested on Manjaro 20.2.1.
+## Tested on Arch 2023-03-01
 ##
 ## Installs:
 ## - Common dependencies and tools for nuttx, jMAVSim
@@ -50,6 +50,7 @@ sudo pacman -Sy --noconfirm --needed \
 	cmake \
 	cppcheck \
 	doxygen \
+	fuse2 \
 	gdb \
 	git \
 	gnutls \
@@ -66,7 +67,7 @@ sudo pacman -Sy --noconfirm --needed \
 
 # Python dependencies
 echo "Installing PX4 Python3 dependencies"
-pip install --user -r ${DIR}/requirements.txt
+pip install --break-system-packages -r ${DIR}/${REQUIREMENTS_FILE}
 
 # NuttX toolchain (arm-none-eabi-gcc)
 if [[ $INSTALL_NUTTX == "true" ]]; then
@@ -74,45 +75,17 @@ if [[ $INSTALL_NUTTX == "true" ]]; then
 	echo "Installing NuttX dependencies"
 
 	sudo pacman -S --noconfirm --needed \
-		gperf \
-		vim \
+		arm-none-eabi-gcc \
+		arm-none-eabi-newlib \
 		;
 
 	if [ ! -z "$USER" ]; then
 		# add user to dialout group (serial port access)
-		sudo usermod -aG uucp $USER
+		sudo echo usermod -aG uucp $USER
 	fi
 
-	# remove modem manager (interferes with PX4 serial port usage)
-	sudo pacman -R modemmanager --noconfirm
-
-	# arm-none-eabi-gcc
-	NUTTX_GCC_VERSION="10-2020-q4-major"
-	NUTTX_GCC_VERSION_SHORT="10-2020q4"
-
-	source $HOME/.profile # load changed path for the case the script is reran before relogin
-	if [ $(which arm-none-eabi-gcc) ]; then
-		GCC_VER_STR=$(arm-none-eabi-gcc --version)
-		GCC_FOUND_VER=$(echo $GCC_VER_STR | grep -c "${NUTTX_GCC_VERSION}")
-	fi
-
-	if [[ "$GCC_FOUND_VER" == "1" ]]; then
-		echo "arm-none-eabi-gcc-${NUTTX_GCC_VERSION} found, skipping installation"
-
-	else
-		echo "Installing arm-none-eabi-gcc-${NUTTX_GCC_VERSION}";
-		wget -O /tmp/gcc-arm-none-eabi-${NUTTX_GCC_VERSION}-linux.tar.bz2 https://armkeil.blob.core.windows.net/developer/Files/downloads/gnu-rm/${NUTTX_GCC_VERSION_SHORT}/gcc-arm-none-eabi-${NUTTX_GCC_VERSION}-x86_64-linux.tar.bz2 && \
-			sudo tar -jxf /tmp/gcc-arm-none-eabi-${NUTTX_GCC_VERSION}-linux.tar.bz2 -C /opt/;
-
-		# add arm-none-eabi-gcc to user's PATH
-		exportline="export PATH=/opt/gcc-arm-none-eabi-${NUTTX_GCC_VERSION}/bin:\$PATH"
-
-		if grep -Fxq "$exportline" $HOME/.profile; then
-			echo "${NUTTX_GCC_VERSION} path already set.";
-		else
-			echo $exportline >> $HOME/.profile;
-		fi
-	fi
+	# don't run modem manager (interferes with PX4 serial port usage)
+	sudo systemctl disable --now ModemManager
 fi
 
 # Simulation tools
@@ -122,8 +95,7 @@ if [[ $INSTALL_SIM == "true" ]]; then
 
 	# java (jmavsim)
 	sudo pacman -S --noconfirm --needed \
-		ant \
-		jdk-openjdk \
+		ant
 		;
 
 	# Gazebo setup
@@ -161,5 +133,5 @@ fi
 
 if [[ $INSTALL_NUTTX == "true" ]]; then
 	echo
-	echo "Reboot or logout, login computer before attempting to build NuttX targets"
+	echo "Reboot or logout, login computer before attempting to flash NuttX targets"
 fi

Tools/setup/macos.sh

@@ -34,6 +34,7 @@ if [[ $REINSTALL_FORMULAS == "--reinstall" ]]; then
 	brew tap PX4/px4
 	brew reinstall px4-dev
 	brew install ncurses
+	brew install python-tk
 else
 	if brew ls --versions px4-dev > /dev/null; then
 		echo "px4-dev already installed"
@@ -42,6 +43,7 @@ else
 		brew tap PX4/px4
 		brew install px4-dev
 		brew install ncurses
+		brew install python-tk
 	fi
 fi
 

Tools/setup/requirements.txt

@@ -2,7 +2,7 @@ argcomplete
 argparse>=1.2
 cerberus
 coverage
-empy>=3.3
+empy==3.3.4
 future
 jinja2>=2.8
 jsonschema

Tools/setup/ubuntu.sh

@@ -155,7 +155,7 @@ if [[ $INSTALL_NUTTX == "true" ]]; then
 
 	if [ -n "$USER" ]; then
 		# add user to dialout group (serial port access)
-		sudo usermod -a -G dialout $USER
+		sudo usermod -aG dialout $USER
 	fi
 
 	# arm-none-eabi-gcc

Tools/simulation/.vscode/c_cpp_properties.json

@@ -0,0 +1,20 @@
+{
+  "configurations": [
+    {
+      "browse": {
+        "databaseFilename": "${default}",
+        "limitSymbolsToIncludedHeaders": false
+      },
+      "includePath": [
+        "/opt/ros/humble/include/**",
+        "/usr/include/**"
+      ],
+      "name": "ROS",
+      "intelliSenseMode": "gcc-x64",
+      "compilerPath": "/usr/bin/gcc",
+      "cStandard": "gnu11",
+      "cppStandard": "c++14"
+    }
+  ],
+  "version": 4
+}

Tools/simulation/.vscode/settings.json

@@ -0,0 +1,10 @@
+{
+    "python.autoComplete.extraPaths": [
+        "/opt/ros/humble/lib/python3.10/site-packages",
+        "/opt/ros/humble/local/lib/python3.10/dist-packages"
+    ],
+    "python.analysis.extraPaths": [
+        "/opt/ros/humble/lib/python3.10/site-packages",
+        "/opt/ros/humble/local/lib/python3.10/dist-packages"
+    ]
+}

Tools/simulation/gz/models/advanced_plane/model.config

@@ -1,14 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>Advanced Plane</name>
-  <version>1.0</version>
-  <sdf version='1.5'>model.sdf</sdf>
-
-  <author>
-   <name>Karthik Srivatsan</name>
-  </author>
-
-  <description>
-    This is a model of a standard plane, which uses the advanced liftdrag plugin.
-  </description>
-</model>

Tools/simulation/gz/models/advanced_plane/model.sdf

@@ -1,578 +0,0 @@
-<?xml version="1.0"?>
-<sdf version='1.5'>
-  <model name='plane'>
-    <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>1</mass>
-        <inertia>
-          <ixx>0.197563</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.1458929</iyy>
-          <iyz>0</iyz>
-          <izz>0.1477</izz>
-        </inertia>
-      </inertial>
-      <collision name='base_link_collision'>
-        <pose>0 0 -0.07 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.47 0.47 0.11</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <max_vel>10</max_vel>
-              <min_depth>0.01</min_depth>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='base_link_visual'>
-        <pose>0.07 0 -0.08 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/body.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-	  <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-      <sensor name="imu_sensor" type="imu">
-        <always_on>1</always_on>
-        <update_rate>250</update_rate>
-      </sensor>
-      <sensor name="air_pressure_sensor" type="air_pressure">
-        <always_on>1</always_on>
-        <update_rate>50</update_rate>
-        <air_pressure>
-          <pressure>
-            <noise type="gaussian">
-              <mean>0</mean>
-              <stddev>0.01</stddev>
-            </noise>
-          </pressure>
-        </air_pressure>
-      </sensor>
-    </link>
-    <link name='rotor_puller'>
-      <pose>0.3 0 0.0 0 1.57 0</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'>
-        <pose>0.0 0 0.0 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.005</length>
-            <radius>0.1</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='rotor_puller_visual'>
-        <pose>0 0 -0.09 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-	  <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_puller_joint' type='revolute'>
-      <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>
-        <use_parent_model_frame>1</use_parent_model_frame>
-      </axis>
-    </joint>
-
-    <link name="left_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.3 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='left_elevon_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/left_aileron.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="right_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 -0.3 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='right_elevon_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/right_aileron.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="left_flap">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.15 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='left_flap_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/left_flap.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="right_flap">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 -0.15 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='right_flap_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/right_flap.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="elevator">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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>
-      <visual name='elevator_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/elevators.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="rudder">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.05 0 0 0 </pose>
-      </inertial>
-      <visual name='rudder_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Advanced%20Plane/tip/files/meshes/rudder.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>1 0 0 1.0</ambient>
-          <diffuse>1 0 0 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <joint name='servo_0' type='revolute'>
-      <parent>base_link</parent>
-      <child>left_elevon</child>
-      <pose>-0.07 0.4 0.08 0.00 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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_0</joint_name>
-      <sub_topic>servo_0</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-    <joint name='servo_1' type='revolute'>
-      <parent>base_link</parent>
-      <child>right_elevon</child>
-      <pose>-0.07 -0.4 0.08 0.00 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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_1</joint_name>
-      <sub_topic>servo_1</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-    <joint name='servo_4' type='revolute'>
-      <parent>base_link</parent>
-      <child>left_flap</child>
-      <pose>-0.07 0.2 0.08 0.00 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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_4</joint_name>
-      <sub_topic>servo_4</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-    <joint name='servo_5' type='revolute'>
-      <parent>base_link</parent>
-      <child>right_flap</child>
-      <pose>-0.07 -0.2 0.08 0.00 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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_5</joint_name>
-      <sub_topic>servo_5</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-    <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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_2</joint_name>
-      <sub_topic>servo_2</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-    <joint name='servo_3' type='revolute'>
-      <parent>base_link</parent>
-      <child>rudder</child>
-      <pose>-0.5 0 0.05 0.00 0 0.0</pose>
-      <axis>
-        <xyz>0 0 1</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-joint-position-controller-system" name="gz::sim::systems::JointPositionController">
-      <joint_name>servo_3</joint_name>
-      <sub_topic>servo_3</sub_topic>
-      <p_gain>10</p_gain>
-      <i_gain>0</i_gain>
-      <d_gain>0</d_gain>
-    </plugin>
-
-    <plugin filename="gz-sim-advanced-lift-drag-system" name="gz::sim::systems::AdvancedLiftDrag">
-      <a0>0.0</a0>
-      <CL0>0.15188</CL0>
-      <AR>6.5</AR>
-      <eff>0.97</eff>
-      <CLa>5.015</CLa>
-      <CD0>0.029</CD0>
-      <Cem0>0.075</Cem0>
-      <Cema>-0.463966</Cema>
-      <CYb>-0.258244</CYb>
-      <Cellb>-0.039250</Cellb>
-      <Cenb>0.100826</Cenb>
-      <CDp>0.0</CDp>
-      <CYp>0.065861</CYp>
-      <CLp>0.0</CLp>
-      <Cellp>-0.487407</Cellp>
-      <Cemp>0.0</Cemp>
-      <Cenp>-0.040416</Cenp>
-      <CDq>0.055166</CDq>
-      <CYq>0.0</CYq>
-      <CLq>7.971792</CLq>
-      <Cellq>0.0</Cellq>
-      <Cemq>-12.140140</Cemq>
-      <Cenq>0.0</Cenq>
-      <CDr>0.0</CDr>
-      <CYr>0.230299</CYr>
-      <CLr>0.0</CLr>
-      <Cellr>0.078165</Cellr>
-      <Cemr>0.0</Cemr>
-      <Cenr>-0.089947</Cenr>
-      <alpha_stall>0.3391428111</alpha_stall>
-      <CLa_stall>-3.85</CLa_stall>
-      <CDa_stall>-0.9233984055</CDa_stall>
-      <Cema_stall>0</Cema_stall>
-      <cp>-0.12 0.0 0.0</cp>
-      <area>0.34</area>
-      <mac>0.22</mac>
-      <air_density>1.2041</air_density>
-      <forward>1 0 0</forward>
-      <upward>0 0 1</upward>
-      <link_name>base_link</link_name>
-      <num_ctrl_surfaces>4</num_ctrl_surfaces>
-      <control_surface>
-        <name>servo_0</name>
-        <index>0</index>
-        <direction>1</direction>
-        <CD_ctrl>-0.000059</CD_ctrl>
-        <CY_ctrl>0.000171</CY_ctrl>
-        <CL_ctrl>-0.011940</CL_ctrl>
-        <Cell_ctrl>-0.003331</Cell_ctrl>
-        <Cem_ctrl>0.001498</Cem_ctrl>
-        <Cen_ctrl>-0.000057</Cen_ctrl>
-      </control_surface>
-      <control_surface>
-        <name>servo_1</name>
-        <direction>1</direction>
-        <index>1</index>
-        <CD_ctrl>-0.000059</CD_ctrl>
-        <CY_ctrl>-0.000171</CY_ctrl>
-        <CL_ctrl>-0.011940</CL_ctrl>
-        <Cell_ctrl>0.003331</Cell_ctrl>
-        <Cem_ctrl>0.001498</Cem_ctrl>
-        <Cen_ctrl>0.000057</Cen_ctrl>
-      </control_surface>
-      <control_surface>
-        <name>servo_2</name>
-        <direction>-1</direction>
-        <index>2</index>
-        <CD_ctrl>0.000274</CD_ctrl>
-        <CY_ctrl>0</CY_ctrl>
-        <CL_ctrl>0.010696</CL_ctrl>
-        <Cell_ctrl>0.0</Cell_ctrl>
-        <Cem_ctrl>-0.025798</Cem_ctrl>
-        <Cen_ctrl>0.0</Cen_ctrl>
-      </control_surface>
-      <control_surface>
-        <name>servo_3</name>
-        <direction>1</direction>
-        <index>3</index>
-        <CD_ctrl>0.0</CD_ctrl>
-        <CY_ctrl>-0.003913</CY_ctrl>
-        <CL_ctrl>0.0</CL_ctrl>
-        <Cell_ctrl>-0.000257</Cell_ctrl>
-        <Cem_ctrl>0.0</Cem_ctrl>
-        <Cen_ctrl>0.001613</Cen_ctrl>
-      </control_surface>
-    </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>0</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
-      <motorType>velocity</motorType>
-
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-  </model>
-</sdf>

Tools/simulation/gz/models/omnicopter/model.config

@@ -1,15 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>Omnicopter</name>
-  <version>1.0</version>
-  <sdf version='1.9'>model.sdf</sdf>
-
-  <author>
-   <name>Jaeyoung Lim</name>
-   <email>jalim@ethz.ch</email>
-  </author>
-
-  <description>
-    Omnicopter model for over actuated system
-  </description>
-</model>

Tools/simulation/gz/models/omnicopter/model.sdf

@@ -1,8 +0,0 @@
-<?xml version="1.0" encoding="UTF-8"?>
-<sdf version='1.9'>
-  <include>
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-      <pose>0 0 0.2 0 0 0</pose>
-      <uri>https://fuel.gazebosim.org/1.0/PX4/models/Omnicopter</uri>
-    </include>
-</sdf>

Tools/simulation/gz/models/px4vision/model.config

@@ -1,15 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>PX4 Vision</name>
-  <version>1.0</version>
-  <sdf version='1.9'>model.sdf</sdf>
-
-  <author>
-   <name>Jaeyoung Lim</name>
-   <email>jaeyoung@auterion.com</email>
-  </author>
-
-  <description>
-    This is a model of the Holybro PX4 Vision
-  </description>
-</model>

Tools/simulation/gz/models/px4vision/model.sdf

@@ -1,10 +0,0 @@
-<?xml version="1.0" encoding="UTF-8"?>
-<sdf version='1.9'>
-  <model name='px4vision'>
-  <include>
-    <uri>
-      https://fuel.gazebosim.org/1.0/PX4/models/PX4 Vision
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-  </include>
-  </model>
-</sdf>

Tools/simulation/gz/models/rc_cessna/meshes/elevators.dae

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Tools/simulation/gz/models/rc_cessna/meshes/left_aileron.dae

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Tools/simulation/gz/models/rc_cessna/meshes/right_aileron.dae

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Tools/simulation/gz/models/rc_cessna/meshes/right_flap.dae

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-                <triangles count="13" material="Material2">
-                    <input offset="0" semantic="VERTEX" source="#ID10" />
-                    <p>0 1 2 2 1 6 8 9 10 1 14 6 10 16 17 16 10 18 18 10 9 8 22 9 6 14 24 16 26 17 24 14 28 17 26 30 24 28 32</p>
-                </triangles>
-                <triangles count="13" material="Material3">
-                    <input offset="0" semantic="VERTEX" source="#ID10" />
-                    <p>3 4 5 7 4 3 11 12 13 7 15 4 12 11 19 19 11 20 21 20 11 12 23 13 25 15 7 21 27 20 29 15 25 31 27 21 33 29 25</p>
-                </triangles>
-            </mesh>
-        </geometry>
-        <geometry id="ID15">
-            <mesh>
-                <source id="ID18">
-                    <float_array id="ID20" count="9">58.97638 60.7874 28.50244 58.93701 66.5748 27.75591 58.97638 60.95635 29.96063</float_array>
-                    <technique_common>
-                        <accessor count="3" source="#ID20" stride="3">
-                            <param name="X" type="float" />
-                            <param name="Y" type="float" />
-                            <param name="Z" type="float" />
-                        </accessor>
-                    </technique_common>
-                </source>
-                <vertices id="ID19">
-                    <input semantic="POSITION" source="#ID18" />
-                </vertices>
-                <lines count="2" material="Material2">
-                    <input offset="0" semantic="VERTEX" source="#ID19" />
-                    <p>1 0 2 1</p>
-                </lines>
-            </mesh>
-        </geometry>
-    </library_geometries>
-    <library_materials>
-        <material id="ID6" name="__White_">
-            <instance_effect url="#ID7" />
-        </material>
-        <material id="ID11" name="__Gray_">
-            <instance_effect url="#ID12" />
-        </material>
-        <material id="ID16" name="edge_color477979255">
-            <instance_effect url="#ID17" />
-        </material>
-    </library_materials>
-    <library_effects>
-        <effect id="ID7">
-            <profile_COMMON>
-                <technique sid="COMMON">
-                    <lambert>
-                        <diffuse>
-                            <color>1 1 1 1</color>
-                        </diffuse>
-                    </lambert>
-                </technique>
-            </profile_COMMON>
-        </effect>
-        <effect id="ID12">
-            <profile_COMMON>
-                <technique sid="COMMON">
-                    <lambert>
-                        <diffuse>
-                            <color>0.5019608 0.5019608 0.5019608 1</color>
-                        </diffuse>
-                    </lambert>
-                </technique>
-            </profile_COMMON>
-        </effect>
-        <effect id="ID17">
-            <profile_COMMON>
-                <technique sid="COMMON">
-                    <constant>
-                        <transparent opaque="A_ONE">
-                            <color>0.1843137 0.3098039 0.3098039 1</color>
-                        </transparent>
-                        <transparency>
-                            <float>1</float>
-                        </transparency>
-                    </constant>
-                </technique>
-            </profile_COMMON>
-        </effect>
-    </library_effects>
-    <scene>
-        <instance_visual_scene url="#ID1" />
-    </scene>
-</COLLADA>

Tools/simulation/gz/models/rc_cessna/model.config

@@ -1,15 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>rc_cessna</name>
-  <version>1.0</version>
-  <sdf version='1.9'>model.sdf</sdf>
-
-  <author>
-   <name>Benjamin Perseghetti</name>
-   <email>bperseghetti@rudislabs.com</email>
-  </author>
-
-  <description>
-    This is a model of an RC Cessna 182.
-  </description>
-</model>

Tools/simulation/gz/models/rc_cessna/model.sdf

@@ -1,824 +0,0 @@
-<?xml version="1.0"?>
-<sdf version='1.9'>
-  <model name='rc_cessna'>
-    <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>1.5</mass>
-        <inertia>
-          <ixx>0.197563</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.1458929</iyy>
-          <iyz>0</iyz>
-          <izz>0.1477</izz>
-        </inertia>
-      </inertial>
-      <collision name='fuselodge_collision'>
-        <pose>-.14 0 0 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.65 .08 0.10</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <max_vel>10</max_vel>
-              <min_depth>0.01</min_depth>
-            </ode>
-          </contact>
-        </surface>
-      </collision>
-      <collision name='wings_collision'>
-        <pose>-0.01 0 0.07 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.1 1.0 0.01</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <max_vel>10</max_vel>
-              <min_depth>0.01</min_depth>
-            </ode>
-          </contact>
-        </surface>
-      </collision>
-      <!-- <visual name='fuselodge_collision_visual'>
-        <pose>-.14 0 0 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.65 .08 0.1</size>
-          </box>
-        </geometry>
-      </visual>
-      <visual name='wings_collision_visual'>
-        <pose>-0.01 0 0.07 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.1 1.0 0.01</size>
-          </box>
-        </geometry>
-      </visual> -->
-      <visual name='base_link_visual'>
-        <pose>0.07 0 -0.08 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/body.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-      <sensor name="imu_sensor" type="imu">
-        <always_on>1</always_on>
-        <update_rate>250</update_rate>
-      </sensor>
-      <sensor name="air_pressure_sensor" type="air_pressure">
-        <always_on>1</always_on>
-        <update_rate>50</update_rate>
-        <air_pressure>
-          <pressure>
-            <noise type="gaussian">
-              <mean>0</mean>
-              <stddev>0.01</stddev>
-            </noise>
-          </pressure>
-        </air_pressure>
-      </sensor>
-    </link>
-    <link name="airspeed">
-      <pose>0 0 0 0 0 0</pose>
-      <inertial>
-        <pose>0 0 0 0 0 0</pose>
-        <mass>0.015</mass>
-        <inertia>
-          <ixx>1e-05</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>1e-05</iyy>
-          <iyz>0</iyz>
-          <izz>1e-05</izz>
-        </inertia>
-      </inertial>
-      <visual name="airspeed_visual">
-        <geometry>
-          <cylinder>
-            <radius>0.01</radius>
-            <length>0.1</length>
-          </cylinder>
-        </geometry>
-        <material>
-          <ambient>0 0 0 1.0</ambient>
-          <diffuse>0 0 0 1.0</diffuse>
-        </material>
-      </visual>
-      <!-- <sensor name="air_speed" type="air_speed">
-        <always_on>1</always_on>
-        <update_rate>5.0</update_rate>
-        <enable_metrics>false</enable_metrics>
-        <air_speed>
-          <airspeed>
-            <noise type="gaussian">
-              <mean>0</mean>
-              <stddev>0.01</stddev>
-            </noise>
-          </airspeed>
-        </air_speed>
-      </sensor> -->
-    </link>
-    <joint name='airspeed_joint' type='fixed'>
-      <child>airspeed</child>
-      <parent>base_link</parent>
-    </joint>
-    <link name='rotor_puller'>
-      <pose>0.22 0 0.0 0 1.57079632679 0</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'>
-        <pose>0 0 0 0 -1.57079632679 0</pose>
-        <geometry>
-          <box>
-            <size>0.005 0.22 0.02</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <!-- <visual name='rotor_puller_collision_visual'>
-        <pose>0 0 0 0 -1.57079632679 0</pose>
-        <geometry>
-          <box>
-            <size>0.005 0.22 0.02</size>
-          </box>
-        </geometry>
-      </visual> -->
-      <visual name='rotor_puller_visual'>
-        <pose>0 0 0 0 0 -1.57079632679</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_puller_joint' type='revolute'>
-      <child>rotor_puller</child>
-      <parent>base_link</parent>
-      <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="left_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.3 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='left_elevon_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/left_aileron.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="LeftWheel">
-      <pose relative_to="LeftWheelJoint">0 0 0 0 0 0</pose>
-      <inertial>
-        <mass>.05</mass>
-        <inertia>
-          <ixx>0.00003331</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.0000204</iyy>
-          <iyz>0</iyz>
-          <izz>0.0000204</izz>
-        </inertia>
-      </inertial>
-      <gravity>true</gravity>
-      <velocity_decay/>
-      <visual name="LeftWheelVisual">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.03</radius>
-          </cylinder>
-        </geometry>
-      </visual>
-      <collision name="LeftWheelCollision">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.03</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <friction>
-            <ode>
-              <mu>1.0</mu>
-              <mu2>0.5</mu2>
-              <fdir1>0 0 1</fdir1>
-            </ode>
-          </friction>
-        </surface>
-      </collision>
-    </link>
-    <link name="RightWheel">
-      <pose relative_to="RightWheelJoint">0 0 0 0 0 0</pose>
-      <inertial>
-        <mass>.05</mass>
-        <inertia>
-          <ixx>0.00003331</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.0000204</iyy>
-          <iyz>0</iyz>
-          <izz>0.0000204</izz>
-        </inertia>
-      </inertial>
-      <gravity>true</gravity>
-      <velocity_decay/>
-      <visual name="RightWheelVisual">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.03</radius>
-          </cylinder>
-        </geometry>
-      </visual>
-      <collision name="RightWheelCollision">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.03</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <friction>
-            <ode>
-              <mu>1.0</mu>
-              <mu2>0.5</mu2>
-              <fdir1>0 0 1</fdir1>
-            </ode>
-          </friction>
-        </surface>
-      </collision>
-    </link>
-    <link name="CenterWheel">
-      <pose relative_to="CenterWheelJoint">0 0 0 0 0 0</pose>
-      <inertial>
-        <mass>.05</mass>
-        <inertia>
-          <ixx>0.00003331</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.0000204</iyy>
-          <iyz>0</iyz>
-          <izz>0.0000204</izz>
-        </inertia>
-      </inertial>
-      <gravity>true</gravity>
-      <velocity_decay/>
-      <visual name="CenterWheelVisual">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.025</radius>
-          </cylinder>
-        </geometry>
-      </visual>
-      <collision name="CenterWheelCollision">
-        <pose>0 0 0 -1.57079632679 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.01</length>
-            <radius>0.025</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <friction>
-            <ode>
-              <mu>1.0</mu>
-              <mu2>0.5</mu2>
-              <fdir1>0 0 1</fdir1>
-            </ode>
-          </friction>
-        </surface>
-      </collision>
-    </link>
-    <link name="right_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 -0.3 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='right_elevon_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/right_aileron.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="left_flap">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.15 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='left_flap_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/left_flap.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="right_flap">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 -0.15 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='right_flap_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/right_flap.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="elevator">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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>
-      <visual name='elevator_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/elevators.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="rudder">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.05 0 0 0 </pose>
-      </inertial>
-      <visual name='rudder_visual'>
-        <pose>0.07 0.0 -0.08 0.00 0 0.0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.1 0.1 0.1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/RC%20Cessna/tip/files/meshes/rudder.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <joint name='servo_0' type='revolute'>
-      <parent>base_link</parent>
-      <child>left_elevon</child>
-      <pose>-0.07 0.4 0.08 0.00 0 0.0</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>-0.07 -0.4 0.08 0.00 0 0.0</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='left_flap_joint' type='revolute'>
-      <parent>base_link</parent>
-      <child>left_flap</child>
-      <pose>-0.07 0.2 0.08 0.00 0 0.0</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='right_flap_joint' type='revolute'>
-      <parent>base_link</parent>
-      <child>right_flap</child>
-      <pose>-0.07 -0.2 0.08 0.00 0 0.0</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>
-    <joint name='rudder_joint' type='revolute'>
-      <parent>base_link</parent>
-      <child>rudder</child>
-      <pose>-0.5 0 0.05 0.00 0 0.0</pose>
-      <axis>
-        <xyz>0 0 1</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="LeftWheelJoint" type="revolute">
-      <parent>base_link</parent>
-      <child>LeftWheel</child>
-      <pose relative_to="base_link">-.035 .13 -0.12 0 0 0</pose>
-      <axis>
-        <xyz>0 1 0</xyz>
-        <limit>
-          <lower>-1.79769e+308</lower>
-          <upper>1.79769e+308</upper>
-        </limit>
-        <dynamics>
-          <spring_reference>0</spring_reference>
-          <spring_stiffness>0</spring_stiffness>
-        </dynamics>
-      </axis>
-    </joint>
-    <joint name="RightWheelJoint" type="revolute">
-      <parent>base_link</parent>
-      <child>RightWheel</child>
-      <pose relative_to="base_link">-.035 -.13 -0.12 0 0 0</pose>
-      <axis>
-        <xyz>0 1 0</xyz>
-        <limit>
-          <lower>-1.79769e+308</lower>
-          <upper>1.79769e+308</upper>
-        </limit>
-        <dynamics>
-          <spring_reference>0</spring_reference>
-          <spring_stiffness>0</spring_stiffness>
-        </dynamics>
-      </axis>
-    </joint>
-    <joint name="CenterWheelJoint" type="revolute">
-      <parent>base_link</parent>
-      <child>CenterWheel</child>
-      <pose relative_to="base_link">.135 0 -0.12 0 0 0</pose>
-      <axis>
-        <xyz>0 1 0</xyz>
-        <limit>
-          <lower>-1.79769e+308</lower>
-          <upper>1.79769e+308</upper>
-        </limit>
-        <dynamics>
-          <spring_reference>0</spring_reference>
-          <spring_stiffness>0</spring_stiffness>
-        </dynamics>
-      </axis>
-    </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 0.45 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>0.05984281113</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 0.15 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>left_flap_joint</control_joint_name>
-      <control_joint_rad_to_cl>-0.1</control_joint_rad_to_cl>
-    </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 -0.15 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>right_flap_joint</control_joint_name>
-      <control_joint_rad_to_cl>-0.1</control_joint_rad_to_cl>
-    </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>rudder_joint</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>rudder_joint</joint_name>
-      <sub_topic>servo_3</sub_topic>
-      <p_gain>10.0</p_gain>
-    </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>1000</maxRotVelocity>
-      <motorConstant>2.44858e-05</motorConstant>
-      <momentConstant>0.016</momentConstant>
-      <commandSubTopic>command/motor_speed</commandSubTopic>
-      <motorNumber>0</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
-      <motorType>velocity</motorType>
-    </plugin>
-    <static>0</static>
-  </model>
-</sdf>

Tools/simulation/gz/models/standard_vtol/model.config

@@ -1,15 +0,0 @@
-<?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>

Tools/simulation/gz/models/standard_vtol/model.sdf

@@ -1,755 +0,0 @@
-<?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>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='base_link_visual'>
-        <pose>0.53 -1.072 -0.1 1.5707963268 0 3.1415926536</pose>
-        <geometry>
-          <mesh>
-            <scale>0.001 0.001 0.001</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/x8_wing.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='left_motor_column'>
-        <pose>0 0.35 0.01 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.74 0.03 0.03</size>
-          </box>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='right_motor_column'>
-        <pose>0 -0.35 0.01 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.74 0.03 0.03</size>
-          </box>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='m0'>
-        <pose>-0.35 0.35 0.045 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.035</length>
-            <radius>0.02</radius>
-          </cylinder>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='m1'>
-        <pose>-0.35 -0.35 0.045 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.035</length>
-            <radius>0.02</radius>
-          </cylinder>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='m2'>
-        <pose>0.35 -0.35 0.045 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.035</length>
-            <radius>0.02</radius>
-          </cylinder>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <visual name='m3'>
-        <pose>0.35 0.35 0.045 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.035</length>
-            <radius>0.02</radius>
-          </cylinder>
-        </geometry>
-        <material>
-          <ambient>.175 .175 .175 1.0</ambient>
-          <diffuse>.175 .175 .175 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-      <sensor name="imu_sensor" type="imu">
-        <always_on>1</always_on>
-        <update_rate>250</update_rate>
-      </sensor>
-      <sensor name="air_pressure_sensor" type="air_pressure">
-        <always_on>1</always_on>
-        <update_rate>50</update_rate>
-        <air_pressure>
-          <pressure>
-            <noise type="gaussian">
-              <mean>0</mean>
-              <stddev>0.01</stddev>
-            </noise>
-          </pressure>
-        </air_pressure>
-      </sensor>
-    </link>
-    <link name='rotor_0'>
-      <pose>0.35 -0.35 0.07 0 0 0</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_0_collision'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.005</length>
-            <radius>0.1</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='rotor_0_visual'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_0_joint' type='revolute'>
-      <child>rotor_0</child>
-      <parent>base_link</parent>
-      <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'>
-      <pose>-0.35 0.35 0.07 0 0 0</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_1_collision'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.005</length>
-            <radius>0.1</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='rotor_1_visual'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_1_joint' type='revolute'>
-      <child>rotor_1</child>
-      <parent>base_link</parent>
-      <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'>
-      <pose>0.35 0.35 0.07 0 0 0</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_2_collision'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.005</length>
-            <radius>0.1</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='rotor_2_visual'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_2_joint' type='revolute'>
-      <child>rotor_2</child>
-      <parent>base_link</parent>
-      <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_3'>
-      <pose>-0.35 -0.35 0.07 0 0 0</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_3_collision'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <cylinder>
-            <length>0.005</length>
-            <radius>0.1</radius>
-          </cylinder>
-        </geometry>
-        <surface>
-          <contact>
-            <ode/>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <visual name='rotor_3_visual'>
-        <pose>0 0 0 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-      <gravity>1</gravity>
-      <velocity_decay/>
-      <self_collide>0</self_collide>
-    </link>
-    <joint name='rotor_3_joint' type='revolute'>
-      <child>rotor_3</child>
-      <parent>base_link</parent>
-      <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>-0.22 0 0.0 0 1.57 0</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'>
-        <pose>0.0 0 -0.04 0 0 0</pose>
-        <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'>
-        <pose>0 0 -0.04 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.8 0.8 0.8</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/iris_prop_ccw.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </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>
-
-    <link name="left_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 0.3 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='left_elevon_visual'>
-        <pose>-0.105 0.004 -0.034 1.5707963268 0 3.1415926536</pose>
-        <geometry>
-          <mesh>
-            <scale>0.001 0.001 0.001</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/x8_elevon_left.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="right_elevon">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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 -0.6 0 0.00 0 0.0</pose>
-      </inertial>
-      <visual name='right_elevon_visual'>
-        <pose>0.281 -1.032 -0.034 1.5707963268 0 3.1415926536</pose>
-        <geometry>
-          <mesh>
-            <scale>0.001 0.001 0.001</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/Standard%20VTOL/tip/files/meshes/x8_elevon_right.dae</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <ambient>0 0 1 1.0</ambient>
-          <diffuse>0 0 1 1.0</diffuse>
-        </material>
-      </visual>
-    </link>
-    <link name="elevator">
-      <inertial>
-        <mass>0.00000001</mass>
-        <inertia>
-          <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>

Tools/simulation/gz/models/x500/model.config

@@ -1,11 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>x500</name>
-  <version>1.0</version>
-  <sdf version="1.9">model.sdf</sdf>
-  <author>
-    <name>Benjamin Perseghetti</name>
-    <email>bperseghetti@rudislabs.com</email>
-  </author>
-  <description>Model of the NXP HoverGames Drone development kit (KIT-HGDRONEK66). The PX4 software compatible kit provides mechanical, RC remote and other components needed to evaluate the RDDRONE-FMUK66 reference design. The FMU includes 100Base-T1 Automotive Ethernet, dual CAN transceivers, as well as SE050 secure element, and works with add on boards NavQPlus, MR-T1ETH8, MR-T1ADAPT, and CAN-nodes such as UCANS32K1SIC.  Kit may be used with, and contains the components needed for the HoverGames.com coding challenges.</description>
-</model>

Tools/simulation/gz/models/x500/model.sdf

@@ -1,588 +0,0 @@
-<?xml version="1.0" encoding="UTF-8"?>
-<sdf version='1.9'>
-  <model name='x500'>
-    <pose>0 0 .24 0 0 0</pose>
-    <self_collide>false</self_collide>
-    <static>false</static>
-    <link name="base_link">
-      <inertial>
-        <mass>2.0</mass>
-        <inertia>
-          <ixx>0.02166666666666667</ixx>
-          <ixy>0</ixy>
-          <ixz>0</ixz>
-          <iyy>0.02166666666666667</iyy>
-          <iyz>0</iyz>
-          <izz>0.04000000000000001</izz>
-        </inertia>
-      </inertial>
-      <gravity>true</gravity>
-      <velocity_decay/>
-      <visual name="base_link_visual">
-        <pose>0 0 .025 0 0 3.141592654</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/NXP-HGD-CF.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <visual name="5010_motor_base_0">
-        <pose>0.174 0.174 .032 0 0 -.45</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Base.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <visual name="5010_motor_base_1">
-        <pose>-0.174 0.174 .032 0 0 -.45</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Base.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <visual name="5010_motor_base_2">
-        <pose>0.174 -0.174 .032 0 0 -.45</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Base.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <visual name="5010_motor_base_3">
-        <pose>-0.174 -0.174 .032 0 0 -.45</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Base.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <visual name="NXP_FMUK66_FRONT">
-        <pose>0.047 .001 .043 1 0 1.57</pose>
-        <cast_shadows>false</cast_shadows>
-        <geometry>
-          <plane>
-            <normal>0 0 1</normal>
-            <size>.013 .007</size>
-          </plane>
-        </geometry>
-        <material>
-          <diffuse>1.0 1.0 1.0</diffuse>
-          <specular>1.0 1.0 1.0</specular>
-          <pbr>
-            <metal>
-              <albedo_map>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/materials/textures/nxp.png</albedo_map>
-            </metal>
-          </pbr>
-        </material>
-      </visual>
-      <visual name="NXP_FMUK66_TOP">
-        <pose>-0.023 0 .0515 0 0 -1.57</pose>
-        <cast_shadows>false</cast_shadows>
-        <geometry>
-          <plane>
-            <normal>0 0 1</normal>
-            <size>.013 .007</size>
-          </plane>
-        </geometry>
-        <material>
-          <diffuse>1.0 1.0 1.0</diffuse>
-          <specular>1.0 1.0 1.0</specular>
-          <pbr>
-            <metal>
-              <albedo_map>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/materials/textures/nxp.png</albedo_map>
-            </metal>
-          </pbr>
-        </material>
-      </visual>
-      <visual name="RDDRONE_FMUK66_TOP">
-        <pose>-.03 0 .0515 0 0 -1.57</pose>
-        <cast_shadows>false</cast_shadows>
-        <geometry>
-          <plane>
-            <normal>0 0 1</normal>
-            <size>.032 .0034</size>
-          </plane>
-        </geometry>
-        <material>
-          <diffuse>1.0 1.0 1.0</diffuse>
-          <specular>1.0 1.0 1.0</specular>
-          <pbr>
-            <metal>
-              <albedo_map>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/materials/textures/rd.png</albedo_map>
-            </metal>
-          </pbr>
-        </material>
-      </visual>
-      <collision name="base_link_collision_0">
-        <pose>0 0 .007 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.35355339059327373 0.35355339059327373 0.05</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <min_depth>0.001</min_depth>
-              <max_vel>0</max_vel>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <collision name="base_link_collision_1">
-        <pose>0 -0.098 -.123 -0.35 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.015 0.015 0.21</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <min_depth>0.001</min_depth>
-              <max_vel>0</max_vel>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <collision name="base_link_collision_2">
-        <pose>0 0.098 -.123 0.35 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.015 0.015 0.21</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <min_depth>0.001</min_depth>
-              <max_vel>0</max_vel>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <collision name="base_link_collision_3">
-        <pose>0 -0.132 -.2195 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.25 0.015 0.015</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <min_depth>0.001</min_depth>
-              <max_vel>0</max_vel>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <collision name="base_link_collision_4">
-        <pose>0 0.132 -.2195 0 0 0</pose>
-        <geometry>
-          <box>
-            <size>0.25 0.015 0.015</size>
-          </box>
-        </geometry>
-        <surface>
-          <contact>
-            <ode>
-              <min_depth>0.001</min_depth>
-              <max_vel>0</max_vel>
-            </ode>
-          </contact>
-          <friction>
-            <ode/>
-          </friction>
-        </surface>
-      </collision>
-      <sensor name="air_pressure_sensor" type="air_pressure">
-        <always_on>1</always_on>
-        <update_rate>50</update_rate>
-        <air_pressure>
-          <pressure>
-            <noise type="gaussian">
-              <mean>0</mean>
-              <stddev>0.01</stddev>
-            </noise>
-          </pressure>
-        </air_pressure>
-      </sensor>
-      <sensor name="imu_sensor" type="imu">
-        <always_on>1</always_on>
-        <update_rate>250</update_rate>
-      </sensor>
-    </link>
-    <link name="rotor_0">
-      <gravity>true</gravity>
-      <self_collide>false</self_collide>
-      <velocity_decay/>
-      <pose>0.174 -0.174 0.06 0 0 0</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">
-        <pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/1345_prop_ccw.stl</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <script>
-            <name>Gazebo/DarkGrey</name>
-            <uri>file://media/materials/scripts/gazebo.material</uri>
-          </script>
-        </material>
-      </visual>
-      <visual name="rotor_0_visual_motor_bell">
-        <pose>0 0 -.032 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Bell.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <collision name="rotor_0_collision">
-        <pose>0 0 0 0 0 0 </pose>
-        <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_1">
-      <gravity>true</gravity>
-      <self_collide>false</self_collide>
-      <velocity_decay/>
-      <pose>-0.174 0.174 0.06 0 0 0</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">
-        <pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/1345_prop_ccw.stl</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <script>
-            <name>Gazebo/DarkGrey</name>
-            <uri>file://media/materials/scripts/gazebo.material</uri>
-          </script>
-        </material>
-      </visual>
-      <visual name="rotor_1_visual_motor_top">
-        <pose>0 0 -.032 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Bell.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <collision name="rotor_1_collision">
-        <pose>0 0 0 0 0 0 </pose>
-        <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_2">
-      <gravity>true</gravity>
-      <self_collide>false</self_collide>
-      <velocity_decay/>
-      <pose>0.174 0.174 0.06 0 0 0</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">
-        <pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/1345_prop_cw.stl</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <script>
-            <name>Gazebo/DarkGrey</name>
-            <uri>file://media/materials/scripts/gazebo.material</uri>
-          </script>
-        </material>
-      </visual>
-      <visual name="rotor_2_visual_motor_top">
-        <pose>0 0 -.032 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Bell.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <collision name="rotor_2_collision">
-        <pose>0 0 0 0 0 0 </pose>
-        <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_3">
-      <gravity>true</gravity>
-      <self_collide>false</self_collide>
-      <velocity_decay/>
-      <pose>-0.174 -0.174 0.06 0 0 0</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">
-        <pose>-0.022 -0.14638461538461536 -0.016 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>0.8461538461538461 0.8461538461538461 0.8461538461538461</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/1345_prop_cw.stl</uri>
-          </mesh>
-        </geometry>
-        <material>
-          <script>
-            <name>Gazebo/DarkGrey</name>
-            <uri>file://media/materials/scripts/gazebo.material</uri>
-          </script>
-        </material>
-      </visual>
-      <visual name="rotor_3_visual_motor_top">
-        <pose>0 0 -.032 0 0 0</pose>
-        <geometry>
-          <mesh>
-            <scale>1 1 1</scale>
-            <uri>https://fuel.gazebosim.org/1.0/PX4/models/x500/1/files/meshes/5010Bell.dae</uri>
-          </mesh>
-        </geometry>
-      </visual>
-      <collision name="rotor_3_collision">
-        <pose>0 0 0 0 0 0 </pose>
-        <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>
-   <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>1000.0</maxRotVelocity>
-      <motorConstant>8.54858e-06</motorConstant>
-      <momentConstant>0.016</momentConstant>
-      <commandSubTopic>command/motor_speed</commandSubTopic>
-      <motorNumber>0</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</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>1000.0</maxRotVelocity>
-      <motorConstant>8.54858e-06</motorConstant>
-      <momentConstant>0.016</momentConstant>
-      <commandSubTopic>command/motor_speed</commandSubTopic>
-      <motorNumber>1</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</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>1000.0</maxRotVelocity>
-      <motorConstant>8.54858e-06</motorConstant>
-      <momentConstant>0.016</momentConstant>
-      <commandSubTopic>command/motor_speed</commandSubTopic>
-      <motorNumber>2</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</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>1000.0</maxRotVelocity>
-      <motorConstant>8.54858e-06</motorConstant>
-      <momentConstant>0.016</momentConstant>
-      <commandSubTopic>command/motor_speed</commandSubTopic>
-      <motorNumber>3</motorNumber>
-      <rotorDragCoefficient>8.06428e-05</rotorDragCoefficient>
-      <rollingMomentCoefficient>1e-06</rollingMomentCoefficient>
-      <rotorVelocitySlowdownSim>10</rotorVelocitySlowdownSim>
-      <motorType>velocity</motorType>
-    </plugin>
-  </model>
-</sdf>

Tools/simulation/gz/models/x500_depth/model.config

@@ -1,11 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>x500-Depth</name>
-  <version>1.0</version>
-  <sdf version="1.9">model.sdf</sdf>
-  <author>
-    <name>Benjamin Perseghetti</name>
-    <email>bperseghetti@rudislabs.com</email>
-  </author>
-  <description>Model of the NXP HoverGames Drone development kit (KIT-HGDRONEK66). The PX4 software compatible kit provides mechanical, RC remote and other components needed to evaluate the RDDRONE-FMUK66 reference design. The FMU includes 100Base-T1 Automotive Ethernet, dual CAN transceivers, as well as SE050 secure element, and works with add on boards NavQPlus, MR-T1ETH8, MR-T1ADAPT, and CAN-nodes such as UCANS32K1SIC.  Kit may be used with, and contains the components needed for the HoverGames.com coding challenges.</description>
-</model>

Tools/simulation/gz/models/x500_depth/model.sdf

@@ -1,17 +0,0 @@
-<?xml version="1.0" encoding="UTF-8"?>
-<sdf version='1.9'>
-  <model name='x500-Depth'>
-    <include merge='true'>
-      <uri>x500</uri>
-    </include>
-    <include merge='true'>
-      <uri>https://fuel.gazebosim.org/1.0/RudisLaboratories/models/OakD-Lite</uri>
-      <pose>.12 .03 .242 0 0 0</pose>
-    </include>
-    <joint name="CameraJoint" type="fixed">
-      <parent>base_link</parent>
-      <child>OakD-Lite/base_link</child>
-      <pose relative_to="base_link">.12 .03 .242 0 0 0</pose>
-    </joint>
-  </model>
-</sdf>

Tools/simulation/gz/models/x500_vision/model.config

@@ -1,11 +0,0 @@
-<?xml version="1.0"?>
-<model>
-  <name>x500-vision</name>
-  <version>1.0</version>
-  <sdf version="1.9">model.sdf</sdf>
-  <author>
-    <name>Jaeyoung Lim</name>
-    <email>jalim@ethz.ch</email>
-  </author>
-  <description>Model of the X500 with a odometry/external vision input.</description>
-</model>

Tools/simulation/gz/models/x500_vision/model.sdf

@@ -1,13 +0,0 @@
-<?xml version="1.0" encoding="UTF-8"?>
-<sdf version='1.9'>
-  <model name='x500-vision'>
-    <include merge='true'>
-      <uri>x500</uri>
-    </include>
-      <plugin
-        filename="gz-sim-odometry-publisher-system"
-        name="gz::sim::systems::OdometryPublisher">
-        <dimensions>3</dimensions>
-      </plugin>
-  </model>
-</sdf>

Tools/simulation/gz/tools/avl_automation/README.md

@@ -1,149 +0,0 @@
-## Purpose
-
-The idea of this tool is to automate the writing of the Advanced Lift Drag plugin by automatizing the coefficient generation and requiring minimal user calculations.
-
-## Setup
-
-In order to run this tool, it is necessary to follow these steps:
-
-1. Download AVL 3.36 from <https://web.mit.edu/drela/Public/web/avl/>. The file for AVL version 3.36 can be found about halfway down the page.
-2. After downloading, extract AVL and move it to the home directory using:
-
-```shell
-sudo tar -xf avl3.36.tgz
-mv ./Avl /home/
-```
-
-Follow the README.md found in Avl to finish the setup process for AVL (requires to set up plotlib and eispack libraries). I recommend using the gfortran compile option. This might require you to install gfortran. This can be done by running:
-
-```shell
-sudo apt update
-sudo apt install gfortran
-```
-
-When running the Makefile for AVL, you might encounter an Error 1 message stating that there is a directory missing. This does not prevent AVL from working for our purposes. Once the process described in the AVL README is completed, AVL is ready to be used. No further set up is required on the side of the AVL or the tool.
-If you want to move the location of the AVL directory, this can simply be done by passing the `--avl_path` flag to the `input_avl.py` file, using the desired directory location for the flag (don't forget to place a "/" behind the last part of the path). Running this will automatically also adjust the paths where necessary.
-
-## Run
-
-To run the tool all that is needed is to modify the `input.yml` to the plane that you desire and then run `python input_avl.py <your_custom_yaml_file>.yml` Note that you require to have the yaml and argparse packages in your python environment to run this. An example template has been provided in the form of the `input.yml` that implements a standard plane with two ailerons, an elevator and a rudder. This example template can be run using: `python input_avl.py --yaml_file input.yml`.
-Once the script has been executed, the generated .avl, .sdf and a plot of the proposed control surfaces can be found in <your-planes-name> directory. The sdf file is the generated Advanced Lift Drag Plugin that can be copied and pasted straight into a model.sdf file, which can then be run in Gazebo.
-
-## Functionality
-
-The tool first asks the user for a range of vehicle specific parameters that are needed in order to specify the geometry and physical properties of the plane. The user has the choice to define a completely custom model, or alternatively select a predefined model template (such as a Cessna or a VTOL), which has a known number of control surfaces, and then provide only some physical properties, without having to define the entire model themselves. The input_avl.py file takes the provided parameter and creates an .avl file from this that can be read by AVL (the program). This happens in the process.sh file. The necessary output generated by AVL will be saved in two files: custom_vehicle_body_axis_derivatives.txt and custom_vehicle_stability_derivatives.txt. These two files contain the parameters that are required in order to populate the Advanced Lift Drag Plugin. Finally, avl_out_parse.py reads the generated .txt files and accordingly assigns parameters to the correct element in sdf. Once this is done, it is only a question of copy and pasting the generated Advanced Lift Drag plugin (found as <custom_plane>.sdf into the desired model.sdf file. )
-
-
-## Usability
-
-The current implementation provides a minimal working example. More accurate measurements can be made by adjusting the chosen number of vortices along span and chord according to desired preferences. A good starting point for this can be found here: <https://www.redalyc.org/pdf/6735/673571173005.pdf>. Furthermore, one can also more accurately model a vehicle by using a larger number of sections. In the current .yml file, only a left and right edge are defined for each surface yielding exactly one section, but the code supports expanding this to any number of desired sections.
-
-## IMPORTANT POINTS TO NOTE
-
-- A control surface in AVL is always defined from left to right. This means you need to first provide the left edge of a surface and then the right edge. If you do this the opposite way around, a surface will essentially be defined upside down.
-- The tool is designed to only support at most two control surfaces of any type on any one vehicle. Having more surfaces than that can lead to faulty behavior.
-- Another important point is that these scripts make use of the match, case syntax, which was only introduced in Python in version 3.10.
-- The primary reference resource for AVL can be found at <https://web.mit.edu/drela/Public/web/avl/AVL_User_Primer.pdf>. This document was written by the creators of AVL and contains all the variables that could be required in defining the control surfaces.
-- AVL cannot predict stall values. As such these need to be calculated/estimated another way. In the current implementation, default stall values have been taken from PX4's Advanced Plane. These should naturally be changed for new/different models.
-
-## Parameter Assignment
-
-Below is a comprehensive list on how the parameters are assigned at output and what files in AVL they are taken from. I am by no means an AVL expert, so please verify that these are actually the correct parameters required by the Advanced Lift Drag Plugin. For an explanation of what the parameters do, please see take a look at the Advanced Lift Drag Plugin.
-
-(name-in-AVL) -> (name-in-plugin)
-
-From the stability derivatives log file, the following advanced lift drag plugin parameters are taken:
-
-Alpha	-> alpha	The angle of attack
-
-Cmtot	-> Cem0		Pitching moment coefficient at zero angle of attack
-
-CLtot	-> CL0		Lift Coefficient at zero angle of attack
-
-CDtot	-> CD0		Drag coefficient at zero angle of attack
-
-CLa	-> CLa		dCL/da (slope of CL-alpha curve)
-
-CYa	-> CYa		dCy/da (sideforce slope wrt alpha)
-
-Cla	-> Cella	dCl/da (roll moment slope wrt alpha)
-
-Cma	-> Cema		dCm/da (pitching moment slope wrt alpha - before stall)
-
-Cna	-> Cena		dCn/da (yaw moment slope wrt alpha)
-
-CLb	-> CLb		dCL/dbeta (lift coefficient slope wrt beta)
-
-CYb	-> CYb		dCY/dbeta (side force slope wrt beta)
-
-Clb	-> Cellb	dCl/dbeta (roll moment slope wrt beta)
-
-Cmb	-> Cemb		dCm/dbeta (pitching moment slope wrt beta)
-
-Cnb	-> Cenb		dCn/dbeta (yaw moment slope wrt beta)
-
-
-From the body axis derivatives log file, the following advanced lift drag plugin parameters are taken:
-
-e	-> eff		Wing efficiency (Oswald efficiency factor for a 3D wing)
-
-CXp	-> CDp		dCD/dp (drag coefficient slope wrt roll rate)
-
-CYp	-> CYp		dCY/dp (sideforce slope wrt roll rate)
-
-CZp	-> CLp		dCL/dp (lift coefficient slope wrt roll rate)
-
-Clp	-> Cellp	dCl/dp (roll moment slope wrt roll rate)
-
-Cmp	-> Cemp		dCm/dp (pitching moment slope wrt roll rate)
-
-Cmp	-> Cenp		dCn/dp (yaw moment slope wrt roll rate)
-
-CXq	-> CDq		dCD/dq (drag coefficient slope wrt pitching rate)
-
-CYq	-> CYq		dCY/dq (side force slope wrt pitching rate)
-
-CZq	-> CLq		dCL/dq (lift coefficient slope wrt pitching rate)
-
-Clq	-> Cellq	dCl/dq (roll moment slope wrt pitching rate)
-
-Cmq	-> Cemq		dCm/dq (pitching moment slope wrt pitching rate)
-
-Cnq	-> Cenq		dCn/dq (yaw moment slope wrt pitching rate)
-
-CXr	-> CDr		dCD/dr (drag coefficient slope wrt yaw rate)
-
-CYr	-> CYr		dCY/dr (side force slope wrt yaw rate)
-
-CZr	-> CLr		dCL/dr (lift coefficient slope wrt yaw rate)
-
-Clr	-> Cellr	dCl/dr (roll moment slope wrt yaw rate)
-
-Cmr	-> Cemr		dCm/dr (pitching moment slope wrt yaw rate)
-
-Cnr	-> Cenr		dCn/dr (yaw moment slope wrt yaw rate)
-
-
-Furthermore, every control surface also has six own parameters, which are also derived from this log file. {i} below ranges from 1 to the number of unique control surface types in the model.
-
-CXd{i}	-> CD_ctrl	Effect of the control surface's deflection on drag
-
-CYd{i}	-> CY_ctrl	Effect of the control surface's deflection on side force
-
-CZd{i}	-> CL_ctrl	Effect of the control surface's deflection on lift
-
-Cld{i}	-> Cell_ctrl	Effect of the control surface's deflection on roll moment
-
-Cmd{i}	-> Cem_ctrl	Effect of the control surface's deflection on pitching moment
-
-Cnd{i}	-> Cen_ctrl	Effect of the control surface's deflection on yaw moment
-
-
-## Future Work
-
-The tool, while self-contained, could be expanded into multiple directions.
-
-1. Currently hinge positions and gains are set at default levels, and these could, if desired be further customized for more control.
-2. More vehicles could be added to provide default templates that require less input. At the moment, only "custom" works completely.
-3. Fuselage modelling could be included to further improve the accuracy of calculated coefficients.
-4. At the moment only NACA airfoils are provided as a way to generate cambered surfaces. An alternative to this would be to use custom airfoil files.

Tools/simulation/gz/tools/avl_automation/avl_out_parse.py

@@ -1,342 +0,0 @@
-#!/usr/bin/env
-
-import argparse
-import shutil
-import fileinput
-import subprocess
-import os
-from typing import TextIO
-
-
-"""
-Get the desired coefficient from the AVL output files by looking through the file line by line and picking it out when encountered.
-
-Args:
-	file (TextIO): The file from which the desired coefficient should be read.
-    token (str): The coefficient which to look for.
-
-Return:
-	value (str): The value associated with the desired coefficient.
-
-"""
-def get_coef(file: TextIO,token: str) -> str:
-
-    linesplit = []
-    for line in file:
-        if f' {token} ' in line:
-            linesplit = line.split()
-            break
-
-    index = 0
-    for i,v in enumerate(linesplit):
-        if v == token:
-            index = i
-    value = linesplit[index+2]
-    return value
-
-
-
-"""
-Write all gathered, model-wide coefficients to the sdf file.
-
-Args:
-	file (TextIO): The file to which the desired coefficient should be written.
-    token_str (str): The coefficients for which the associated value should be written.
-    token (str): The value which should be placed in the avl.
-
-Return:
-	None.
-
-"""
-def write_coef(file: TextIO, token_str: str, token: str):
-    old_line = f'<{token_str}></{token_str}>'
-    new_line = f'<{token_str}>{token}</{token_str}>'
-    with fileinput.FileInput(file, inplace=True) as output_file:
-        for line in output_file:
-            print(line.replace(old_line, new_line), end='')
-
-
-
-"""
-Write all gathered, control surface specific parameters to the sdf file.
-
-Args:
-	file (TextIO): The file to which the desired coefficients should be written.
-    ctrl_surface_vec (list): A vector that contains all 6 necessary coefficient values for the control surface in question.
-    index (str): The model-wide index number of the control surface in question.
-	direction (str): The direction in which the control surface can be actuated.
-
-Return:
-	None.
-"""
-def ctrl_surface_coef(file: TextIO,ctrl_surface_vec: list,index: str, direction: str):
-
-    extracted_text = ''
-    with open("./templates/control_surface.sdf",'r') as open_file:
-        for line in open_file:
-            extracted_text += line
-        open_file.close()
-
-	# Insert necessary coefficient values, index and direction in correct sdf location.
-    extracted_text = extracted_text.replace("<name></name>",f'<name>servo_{index}</name>')
-    extracted_text = extracted_text.replace("<index></index>",f'<index>{index}</index>')
-    extracted_text = extracted_text.replace("<direction></direction>",f'<directon>{direction}</direction>')
-    extracted_text = extracted_text.replace("<CD_ctrl></CD_ctrl>",f'<CD_ctrl>{ctrl_surface_vec[0]}</CD_ctrl>')
-    extracted_text = extracted_text.replace("<CY_ctrl></CY_ctrl>",f'<CY_ctrl>{ctrl_surface_vec[1]}</CY_ctrl>')
-    extracted_text = extracted_text.replace("<CL_ctrl></CL_ctrl>",f'<CL_ctrl>{ctrl_surface_vec[2]}</CL_ctrl>')
-    extracted_text = extracted_text.replace("<Cell_ctrl></Cell_ctrl>",f'<Cell_ctrl>{ctrl_surface_vec[3]}</Cell_ctrl>')
-    extracted_text = extracted_text.replace("<Cem_ctrl></Cem_ctrl>",f'<Cem_ctrl>{ctrl_surface_vec[4]}</Cem_ctrl>')
-    extracted_text = extracted_text.replace("<Cen_ctrl></Cen_ctrl>",f'<Cen_ctrl>{ctrl_surface_vec[5]}</Cen_ctrl>')
-
-
-    # Create model specific template
-    with open(file,'a') as plugin_file:
-        plugin_file.write(extracted_text + "\n")
-        plugin_file.close()
-
-"""
-Read out the necessary log files to gather the desired parameters and write them to the sdf plugin file.
-Arguments provided here are passed in the input_avl.py file.
-
-Args:
-	file_name (TextIO): The file to which the desired coefficients should be written.
-    vehicle_type (str): The type of vehicle in use.
-    AR (str): The calculated aspect ratio.
-    mac (str): The calculated mean aerodynamic chord.
-    ref_pt_x (str): The x coordinate of the reference point, at which forces and moments are applied.
-    ref_pt_y (str): The y coordinate of the reference point, at which forces and moments are applied.
-    ref_pt_z (str): The z coordinate of the reference point, at which forces and moments are applied.
-    num_ctrl_surfaces (str): The number of control surfaces that the model uses.
-    area (str): The wing surface area.
-	ctrl_surface_order (list): A list containing the types of control surfaces, in theorder in which
-    	they have been defined in the .avl file.
-    avl_path (str): A string containing the directory where the AVL directory should be moved to.
-
-Return:
-	None.
-"""
-
-def main(file_name: TextIO, vehicle_type: str, AR: str, mac: str, ref_pt_x: str, ref_pt_y: str, ref_pt_z: str, num_ctrl_surfaces: str, area: str, ctrl_surface_order: list, avl_path:str):
-
-	# Set current path for user
-    curr_path = subprocess.run(['pwd'], stdout=subprocess.PIPE, stderr=subprocess.PIPE, text=True)
-
-    if curr_path.returncode == 0:
-        # Save the output in a variable
-        savedir = curr_path.stdout.strip()
-    else:
-        raise LookupError("Invalid path to directory. Check both the avl_automation directory and the Avl directory are positioned correctly.")
-
-	# Set the file directory path from where the AVL output logs can be read.
-    filedir = f'{avl_path}Avl/runs/'
-
-	# Read out all necessary parameters from the stability and body axis derivatives files.
-    with open(f'{filedir}custom_vehicle_stability_derivatives.txt','r+') as stability_file:
-        original_position = stability_file.tell()
-
-        # As plane is modelled at 0 degree AoA, the total coefficients should(?) correspond to the
-        # 0 degree coefficients required by the plugin.
-        alpha = get_coef(stability_file,"Alpha")
-        Cem0 = get_coef(stability_file,"Cmtot")
-        CL0 = get_coef(stability_file,"CLtot")
-        CD0 = get_coef(stability_file,"CDtot")
-
-        CLa = get_coef(stability_file,"CLa")
-        CYa = get_coef(stability_file,"CYa")
-        Cella = get_coef(stability_file,"Cla")
-        Cema = get_coef(stability_file,"Cma")
-        Cena = get_coef(stability_file,"Cna")
-
-        stability_file.seek(original_position)
-
-        CLb = get_coef(stability_file,"CLb")
-        CYb = get_coef(stability_file,"CYb")
-        Cellb = get_coef(stability_file,"Clb")
-        Cemb = get_coef(stability_file,"Cmb")
-        Cenb = get_coef(stability_file,"Cnb")
-        stability_file.close()
-
-    with open(f'{filedir}custom_vehicle_body_axis_derivatives.txt') as bodyax_file:
-        original_position = bodyax_file.tell()
-
-        eff = get_coef(bodyax_file,"e")
-
-        bodyax_file.seek(original_position)
-
-        CDp = get_coef(bodyax_file,"CXp")
-        CYp = get_coef(bodyax_file,"CYp")
-        CLp = get_coef(bodyax_file,"CZp")
-        Cellp = get_coef(bodyax_file,"Clp")
-        Cemp = get_coef(bodyax_file,"Cmp")
-        Cenp = get_coef(bodyax_file,"Cnp")
-
-        bodyax_file.seek(original_position)
-
-        CDq = get_coef(bodyax_file,"CXq")
-        CYq = get_coef(bodyax_file,"CYq")
-        CLq = get_coef(bodyax_file,"CZq")
-        Cellq = get_coef(bodyax_file,"Clq")
-        Cemq = get_coef(bodyax_file,"Cmq")
-        Cenq = get_coef(bodyax_file,"Cnq")
-
-        bodyax_file.seek(original_position)
-
-        CDr = get_coef(bodyax_file,"CXr")
-        CYr = get_coef(bodyax_file,"CYr")
-        CLr = get_coef(bodyax_file,"CZr")
-        Cellr = get_coef(bodyax_file,"Clr")
-        Cemr = get_coef(bodyax_file,"Cmr")
-        Cenr = get_coef(bodyax_file,"Cnr")
-        bodyax_file.close()
-
-    plane_type = vehicle_type
-    ctrl_surface_mat = []
-
-	# Maybe in the future you want more types of set aircraft. Thus us a case differentiator.
-    match plane_type:
-
-        case "custom":
-            ctrl_surface_vec = []
-            with open(f'{filedir}custom_vehicle_body_axis_derivatives.txt') as bodyax_file:
-                original_position = bodyax_file.tell()
-                for i in range(1,(len(set(ctrl_surface_order)))+1):
-                    ctrl_surface_vec = []
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'CXd{i}'))
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'CYd{i}'))
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'CZd{i}'))
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'Cld{i}'))
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'Cmd{i}'))
-                    ctrl_surface_vec.append(get_coef(bodyax_file,f'Cnd{i}'))
-                    bodyax_file.seek(original_position)
-                    ctrl_surface_mat.append(ctrl_surface_vec)
-
-
-	# SPECIFY STALL PARAMETERS BASED ON AIRCRAFT TYPE (IF PROVIDED)
-    if not os.path.exists(f'{savedir}/{file_name}'):
-        os.makedirs(f'{savedir}/{file_name}')
-    file_name = f'{savedir}/{file_name}/{file_name}.sdf'
-    shutil.copy(f'{savedir}/templates/advanced_lift_drag_template.sdf',file_name)
-
-    # Get argument coefficients taken directly from the input file.
-    write_coef(file_name,"a0",alpha)
-    write_coef(file_name,"CL0",CL0)
-    write_coef(file_name,"CD0",CD0)
-    write_coef(file_name,"Cem0",Cem0)
-    write_coef(file_name,"AR",AR)
-    write_coef(file_name,"area",area)
-    write_coef(file_name,"mac",mac)
-    write_coef(file_name,"air_density",1.2041) # TODO: Provide custom air density option
-    write_coef(file_name,"forward","1 0 0")
-    write_coef(file_name,"upward","0 0 1")
-    write_coef(file_name,"link_name","base_link")
-    write_coef(file_name,"cp",f'{ref_pt_x} {ref_pt_y} {ref_pt_z}')
-    write_coef(file_name,"num_ctrl_surfaces",num_ctrl_surfaces)
-
-    write_coef(file_name,"CLa",CLa)
-    write_coef(file_name,"CYa",CYa)
-    write_coef(file_name,"Cella",Cella)
-    write_coef(file_name,"Cema",Cema)
-    write_coef(file_name,"Cena",Cena)
-    write_coef(file_name,"CLb",CLb)
-    write_coef(file_name,"CYb",CYb)
-    write_coef(file_name,"Cellb",Cellb)
-    write_coef(file_name,"Cemb",Cemb)
-    write_coef(file_name,"Cenb",Cenb)
-
-    write_coef(file_name,"CDp",CDp)
-    write_coef(file_name,"CYp",CYp)
-    write_coef(file_name,"CLp",CLp)
-    write_coef(file_name,"Cellp",Cellp)
-    write_coef(file_name,"Cemp",Cemp)
-    write_coef(file_name,"Cenp",Cenp)
-    write_coef(file_name,"CDq",CDq)
-    write_coef(file_name,"CYq",CYq)
-    write_coef(file_name,"CLq",CLq)
-    write_coef(file_name,"Cellq",Cellq)
-    write_coef(file_name,"Cemq",Cemq)
-    write_coef(file_name,"Cenq",Cenq)
-    write_coef(file_name,"CDr",CDr)
-    write_coef(file_name,"CYr",CYr)
-    write_coef(file_name,"CLr",CLr)
-    write_coef(file_name,"Cellr",Cellr)
-    write_coef(file_name,"Cemr",Cemr)
-    write_coef(file_name,"Cenr",Cenr)
-
-    write_coef(file_name,"eff",eff)
-
-    # TODO: Improve this for custom stall values
-    # Note: Currently these stall values are simply taken from advanced_plane presets.
-
-    write_coef(file_name,"alpha_stall","0.3391428111")
-    write_coef(file_name,"CLa_stall","-3.85")
-    write_coef(file_name,"CDa_stall","-0.9233984055")
-    write_coef(file_name,"Cema_stall","0")
-
-    # Check whether a particular type of control surface has been seen before. If it has,
-    # then the current control surface is the (right) counterpart.
-
-    # ASSUMPTION: There is the assumption that an vehicle will only ever have two of any
-    # particular type of control surface. (left and right). If this is not the case, the negation
-    # below will likely not work correctly.
-    type_seen = list()
-
-    # Dictionary containing the directions that each type of control surface can move.
-    ctrl_direction = {"aileron": 1,"elevator": -1,"rudder": 1}
-
-	# More set types in the future?
-    match plane_type:
-
-        case "custom":
-            for i, ctrl_surface in enumerate(ctrl_surface_order):
-
-                # Check whether a particular type of control surface has been seen before. If it has,
-                # then the current control surface is the (right) counterpart. Depending on the exact
-                # nature of the encountered type you then need to negate the correct parameters.
-                if ctrl_surface in type_seen:
-                    # Work out what the corresponding index for the first encounter of the ctrl surface is.
-                    seen_index = type_seen.index(ctrl_surface)
-
-                    if ctrl_surface == 'aileron':
-                        #Change for right wing aileron by flipping sign
-                        ctrl_surface_mat[seen_index][3] = -float(ctrl_surface_mat[0][3])
-                        ctrl_surface_mat[seen_index][5] = -float(ctrl_surface_mat[0][5])
-
-                    # Split Elevators are assumed to never run differentially. Feel free to add a
-                    # condition if your plane does require differential elevator action.
-
-                else:
-                    # If a ctrl surface has not been encountered add it to the type_seen list and
-                    # set the index to the length of the list - 1 as this corresponds to the newest
-                    # unseen element in ctrl_surface_mat .
-                    type_seen.append(ctrl_surface)
-                    seen_index = len(type_seen) - 1
-
-                ctrl_surface_coef(file_name,ctrl_surface_mat[seen_index],i,ctrl_direction[ctrl_surface])
-
-
-    # close the sdf file with plugin
-    with open(file_name,'a') as plugin_file:
-        plugin_file.write("</plugin>")
-        plugin_file.close()
-
-
-if __name__ == '__main__':
-    parser = argparse.ArgumentParser()
-
-    parser.add_argument("file_name", help="The file to which the desired coefficients should be written.")
-    parser.add_argument("vehicle_type", help="The type of vehicle in use.")
-    parser.add_argument("AR", help="The calculated aspect ratio.")
-    parser.add_argument("mac", help="The calculated mean aerodynamic chord.")
-    parser.add_argument("ref_pt_x", help="The x coordinate of the reference point, at which forces and moments are applied.")
-    parser.add_argument("ref_pt_y", help="The y coordinate of the reference point, at which forces and moments are applied.")
-    parser.add_argument("ref_pt_z", help="The z coordinate of the reference point, at which forces and moments are applied.")
-    parser.add_argument("num_ctrl_surfaces", help="The number of control surfaces that the model uses.")
-    parser.add_argument("area", help= "The wing surface area.")
-    parser.add_argument("ctrl_surface_order", help=" A list containing the types of control surfaces, in theorder in which \
-    	they have been defined in the .avl file.")
-    parser.add_argument("avl_path",help="A string containing the directory where the AVL directory should be moved to.")
-
-    args = parser.parse_args()
-
-    main(args.file_name,args.vehicle_type,args.AR,args.mac,args.ref_pt_x,args.ref_pt_y,
-         args.ref_pt_z,args.num_ctrl_surfaces,args.area,args.ctrl_surface_order,args.avl_path)

Tools/simulation/gz/tools/avl_automation/avl_steps.txt

@@ -1,10 +0,0 @@
-oper
-x
-n custom_plane
-st custom_vehicle_stability_derivatives.txt
-sb custom_vehicle_body_axis_derivatives.txt
-g
-h
-
-
-quit

Tools/simulation/gz/tools/avl_automation/input.yml

@@ -1,142 +0,0 @@
-# Enter a name for your vehicle
-vehicle_name: plane_example_2
-
-# Enter the type of airframe you would like to use:
-frame_type: custom
-
-# First define some model-wide parameters for custom models:
-reference_area: 12
-wing_span: 15
-# Provide a reference point at which the forces and moments generated will act.
-reference_point:
-  X: 0
-  Y: 0
-  Z: 0
-
-#Provide information on each of the Control Surfaces
-num_ctrl_surfaces: 4
-control_surfaces:
-  - name: right_wing
-    type: aileron
-    nchord: 1
-    cspace: 1
-    nspan: 16
-    sspace: -2
-    angle: 4
-    translation:
-      X: 0
-      Y: 0
-      Z: 0
-    naca: 2412
-    sections:
-    - name: section_1
-      position:
-        X: -0.25
-        Y: 0
-        Z: 0
-      chord: 1
-      ainc: 0
-      nspan: 8
-      sspace: 1
-    - name: section_2
-      position:
-        X: -0.175
-        Y: 5
-        Z: 0.5
-      chord: 0.7
-      ainc: 0
-      nspan: 0
-      sspace: 0
-
-
-  - name: left_wing
-    type: aileron
-    nchord: 1
-    cspace: 1
-    nspan: 16
-    sspace: -2
-    angle: 4
-    translation:
-      X: 0
-      Y: 0
-      Z: 0
-    naca: 2412
-    sections:
-    - name: section_1
-      position:
-        X: -0.175
-        Y: -5
-        Z: 0.5
-      chord: 0.7
-      ainc: 0
-      nspan: 0
-      sspace: 0
-    - name: section_2
-      position:
-        X: -0.25
-        Y: 0
-        Z: 0
-      chord: 1
-      ainc: 0
-      nspan: 8
-      sspace: 1
-
-  - name: elevator
-    type: elevator
-    nchord: 1
-    cspace: 1
-    nspan: 7
-    sspace: -2
-    translation:
-      X: 6
-      Y: 0
-      Z: 0.5
-    sections:
-    - name: section_1
-      position:
-        X: -0.1
-        Y: 0
-        Z: 0
-      chord: 0.4
-      ainc: 0
-      nspan: 7
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