forked from Archive/PX4-Autopilot
Changed constant name to UNMANNED_GROUND_VEHICLE
This commit is contained in:
parent
714c90b9db
commit
21760a5856
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@ -3,7 +3,7 @@
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# @name Rover
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#
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sh /etc/init.d/rc.ugv_defaults
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sh /etc/init.d/rc.rover_defaults
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if [ $AUTOCNF = yes ]
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then
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@ -229,7 +229,7 @@ fi
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# Configure vehicle type specific parameters.
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# Note: rc.vehicle_setup is the entry point for rc.interface,
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# rc.fw_apps, rc.mc_apps, rc.ugv_apps, and rc.vtol_apps.
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# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
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#
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sh etc/init.d/rc.vehicle_setup
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@ -43,8 +43,8 @@ px4_add_romfs_files(
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rcS
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rc.sensors
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rc.thermal_cal
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rc.ugv_apps
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rc.ugv_defaults
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rc.rover_apps
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rc.rover_defaults
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rc.vehicle_setup
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rc.vtol_apps
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rc.vtol_defaults
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@ -13,7 +13,7 @@
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# @board px4_fmu-v2 exclude
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#
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sh /etc/init.d/rc.ugv_defaults
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sh /etc/init.d/rc.rover_defaults
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if [ $AUTOCNF = yes ]
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then
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@ -54,10 +54,10 @@ then
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param set PWM_MIN 1000
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fi
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# Configure this as ugv
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# Configure this as rover
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set MAV_TYPE 10
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# Set mixer
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set MIXER ugv_generic
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set MIXER rover_generic
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set PWM_MAIN_REV2 1
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@ -17,7 +17,7 @@
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# @board px4_fmu-v2 exclude
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#
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sh /etc/init.d/rc.ugv_defaults
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sh /etc/init.d/rc.rover_defaults
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#
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# This section can be enabled once tuning parameters for this particular
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@ -15,7 +15,7 @@
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# @board px4_fmu-v2 exclude
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#
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sh /etc/init.d/rc.ugv_defaults
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sh /etc/init.d/rc.rover_defaults
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if [ $AUTOCNF = yes ]
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then
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@ -56,7 +56,7 @@ then
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param set PWM_MIN 1000
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fi
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# Configure this as ugv
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# Configure this as rover
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set MAV_TYPE 10
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# Set mixer
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@ -23,4 +23,4 @@ gnd_pos_control start
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#
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# Start Land Detector.
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#
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land_detector start ugv
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land_detector start rover
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@ -5,7 +5,7 @@
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# NOTE: Script variables are declared/initialized/unset in the rcS script.
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#
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set VEHICLE_TYPE ugv
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set VEHICLE_TYPE rover
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if [ $AUTOCNF = yes ]
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then
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@ -87,12 +87,12 @@ fi
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#
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# UGV setup.
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#
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if [ $VEHICLE_TYPE = ugv ]
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if [ $VEHICLE_TYPE = rover ]
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then
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if [ $MIXER = none ]
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then
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# Set default mixer for UGV if not defined.
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set MIXER ugv_generic
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set MIXER rover_generic
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fi
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if [ $MAV_TYPE = none ]
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@ -108,7 +108,7 @@ then
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sh /etc/init.d/rc.interface
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# Start standard UGV apps.
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sh /etc/init.d/rc.ugv_apps
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sh /etc/init.d/rc.rover_apps
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fi
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#
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@ -421,7 +421,7 @@ else
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#
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# Configure vehicle type specific parameters.
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# Note: rc.vehicle_setup is the entry point for rc.interface,
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# rc.fw_apps, rc.mc_apps, rc.ugv_apps, and rc.vtol_apps.
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# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
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#
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sh /etc/init.d/rc.vehicle_setup
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@ -78,7 +78,7 @@ px4_add_romfs_files(
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stampede.main.mix
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tri_y_yaw-.main.mix
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tri_y_yaw+.main.mix
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ugv_generic.main.mix
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rover_generic.main.mix
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Viper.main.mix
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vtol_AAERT.aux.mix
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vtol_AAVVT.aux.mix
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@ -44,7 +44,7 @@ px4_add_romfs_files(
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quad_+.main.mix
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quad_test.mix
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quad_+_vtol.main.mix
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ugv_generic.main.mix
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rover_generic.main.mix
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vtol1_test.mix
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vtol2_test.mix
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vtol_AAERT.aux.mix
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@ -52,7 +52,7 @@ uint8 RC_IN_MODE_GENERATED = 2
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uint8 VEHICLE_TYPE_UNKNOWN = 0
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uint8 VEHICLE_TYPE_ROTARY_WING = 1
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uint8 VEHICLE_TYPE_FIXED_WING = 2
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uint8 VEHICLE_TYPE_GROUND = 3
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uint8 VEHICLE_TYPE_ROVER = 3
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# state machine / state of vehicle.
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# Encodes the complete system state and is set by the commander app.
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@ -67,6 +67,8 @@ uint8 system_id # system id, contains MAVLink's system ID field
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uint8 component_id # subsystem / component id, contains MAVLink's component ID field
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uint8 vehicle_type # Type of vehicle (fixed-wing, rotary wing, ground)
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# If the vehicle is a VTOL, then this value will be VEHICLE_TYPE_ROTARY_WING while flying as a multicopter,
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# and VEHICLE_TYPE_FIXED_WING when flying as a fixed-wing
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bool is_vtol # True if the system is VTOL capable
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bool vtol_fw_permanent_stab # True if VTOL should stabilize attitude for fw in manual mode
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@ -1297,7 +1297,7 @@ Commander::run()
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
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} else if (is_ground_rover(&status)) {
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_GROUND;
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_ROVER;
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} else {
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_UNKNOWN;
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@ -1407,9 +1407,9 @@ Commander::run()
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status.system_type = (uint8_t)system_type;
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}
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bool is_rotary = is_rotary_wing(&status) || (is_vtol(&status) && vtol_status.vtol_in_rw_mode);
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bool is_fixed = is_fixed_wing(&status) || (is_vtol(&status) && !vtol_status.vtol_in_rw_mode);
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bool is_ground = is_ground_rover(&status);
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const bool is_rotary = is_rotary_wing(&status) || (is_vtol(&status) && vtol_status.vtol_in_rw_mode);
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const bool is_fixed = is_fixed_wing(&status) || (is_vtol(&status) && !vtol_status.vtol_in_rw_mode);
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const bool is_ground = is_ground_rover(&status);
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/* disable manual override for all systems that rely on electronic stabilization */
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if (is_rotary) {
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@ -1419,7 +1419,7 @@ Commander::run()
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
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} else if (is_ground) {
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_GROUND;
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_ROVER;
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}
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/* set vehicle_status.is_vtol flag */
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@ -1642,9 +1642,11 @@ Commander::run()
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if (is_vtol(&status)) {
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// Check if there has been any change while updating the flags
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bool is_rotary = status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
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const auto new_vehicle_type = vtol_status.vtol_in_rw_mode ?
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vehicle_status_s::VEHICLE_TYPE_ROTARY_WING :
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vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
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if (is_rotary != vtol_status.vtol_in_rw_mode) {
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if (new_vehicle_type != status.vehicle_type) {
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status.vehicle_type = vtol_status.vtol_in_rw_mode ?
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vehicle_status_s::VEHICLE_TYPE_ROTARY_WING :
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vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
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@ -507,7 +507,7 @@ bool StateMachineHelperTest::mainStateTransitionTest()
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struct vehicle_status_flags_s current_status_flags = {};
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current_commander_state.main_state = test->from_state;
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current_vehicle_status.vehicle_type = test->condition_bits & MTT_ROTARY_WING ?
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current_vehicle_status.vehicle_type = (test->condition_bits & MTT_ROTARY_WING) ?
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vehicle_status_s::VEHICLE_TYPE_ROTARY_WING : vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
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current_status_flags.condition_local_altitude_valid = test->condition_bits & MTT_LOC_ALT_VALID;
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current_status_flags.condition_local_position_valid = test->condition_bits & MTT_LOC_POS_VALID;
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@ -691,6 +691,7 @@ bool set_nav_state(vehicle_status_s *status, actuator_armed_s *armed, commander_
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status->nav_state = vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER;
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} else if (status_flags.condition_local_altitude_valid) {
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//TODO: Add case for rover
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if (status->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
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status->nav_state = vehicle_status_s::NAVIGATION_STATE_DESCEND;
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@ -76,7 +76,7 @@ int LandDetector::task_spawn(int argc, char *argv[])
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} else if (strcmp(argv[1], "vtol") == 0) {
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obj = new VtolLandDetector();
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} else if (strcmp(argv[1], "ugv") == 0) {
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} else if (strcmp(argv[1], "rover") == 0) {
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obj = new RoverLandDetector();
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} else {
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@ -165,7 +165,7 @@ The module runs periodically on the HP work queue.
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PRINT_MODULE_USAGE_NAME("land_detector", "system");
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PRINT_MODULE_USAGE_COMMAND_DESCR("start", "Start the background task");
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PRINT_MODULE_USAGE_ARG("fixedwing|multicopter|vtol|ugv", "Select vehicle type", false);
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PRINT_MODULE_USAGE_ARG("fixedwing|multicopter|vtol|rover", "Select vehicle type", false);
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PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
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return 0;
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}
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@ -335,10 +335,12 @@ MissionBlock::is_mission_item_reached()
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&& PX4_ISFINITE(_mission_item.yaw))) {
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/* check course if defined only for rotary wing except takeoff */
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float cog = _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
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? _navigator->get_global_position()->yaw : atan2f(
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float cog = (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) ?
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_navigator->get_global_position()->yaw :
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atan2f(
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_navigator->get_global_position()->vel_e,
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_navigator->get_global_position()->vel_n);
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_navigator->get_global_position()->vel_n
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);
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float yaw_err = wrap_pi(_mission_item.yaw - cog);
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