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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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9 Commits
| Author | SHA1 | Date | |
|---|---|---|---|
| eebc930a9d | |||
| 4294b148aa | |||
| 49de25f804 | |||
| f01e82f285 | |||
| b2220ea9fa | |||
| defaf72630 | |||
| dddfb8df6d | |||
| ad4ae52cb1 | |||
| 93af9e3923 |
@@ -40,7 +40,7 @@ uint8 NAVIGATION_STATE_AUTO_MISSION = 3 # Auto mission mode
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||||
uint8 NAVIGATION_STATE_AUTO_LOITER = 4 # Auto loiter mode
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uint8 NAVIGATION_STATE_AUTO_RTL = 5 # Auto return to launch mode
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uint8 NAVIGATION_STATE_POSITION_SLOW = 6
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uint8 NAVIGATION_STATE_FREE5 = 7
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uint8 NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING = 7 # Auto dead-reckoning return to launch mode
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uint8 NAVIGATION_STATE_FREE4 = 8
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uint8 NAVIGATION_STATE_FREE3 = 9
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uint8 NAVIGATION_STATE_ACRO = 10 # Acro mode
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@@ -421,18 +421,22 @@
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"description": "RTL"
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},
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"7": {
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"name": "dead_reckon_rtl",
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"description": "Dead Reckoning RTL"
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},
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"8": {
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"name": "land",
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"description": "Land"
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},
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"8": {
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"9": {
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"name": "descend",
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"description": "Descend"
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},
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"9": {
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"10": {
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"name": "disarm",
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"description": "disarm"
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},
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||||
"10": {
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"11": {
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||||
"name": "terminate",
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"description": "terminate"
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}
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@@ -604,6 +608,10 @@
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"name": "external8",
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"description": "External 8"
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},
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"24": {
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"name": "auto_rtl_dr",
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"description": "Dead-Reckoning RTL"
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},
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"255": {
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"name": "unknown",
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"description": "[Unknown]"
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@@ -52,6 +52,7 @@ static inline uint32_t getValidNavStates()
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(1u << vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER) |
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(1u << vehicle_status_s::NAVIGATION_STATE_AUTO_RTL) |
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(1u << vehicle_status_s::NAVIGATION_STATE_POSITION_SLOW) |
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(1u << vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING) |
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(1u << vehicle_status_s::NAVIGATION_STATE_ACRO) |
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(1u << vehicle_status_s::NAVIGATION_STATE_TERMINATION) |
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(1u << vehicle_status_s::NAVIGATION_STATE_OFFBOARD) |
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@@ -74,7 +75,7 @@ const char *const nav_state_names[vehicle_status_s::NAVIGATION_STATE_MAX] = {
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"Hold",
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"Return",
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"Position Slow",
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"7: unallocated",
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"Dead-Reckoning Return",
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"8: unallocated",
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"9: unallocated",
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"Acro",
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@@ -106,6 +106,7 @@ void getVehicleControlMode(uint8_t nav_state, uint8_t vehicle_type,
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vehicle_control_mode.flag_control_allocation_enabled = true;
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break;
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case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING:
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case vehicle_status_s::NAVIGATION_STATE_DESCEND:
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vehicle_control_mode.flag_control_auto_enabled = true;
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vehicle_control_mode.flag_control_climb_rate_enabled = true;
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@@ -133,6 +133,12 @@ void getModeRequirements(uint8_t vehicle_type, failsafe_flags_s &flags)
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL, flags.mode_req_home_position);
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL, flags.mode_req_prevent_arming);
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// NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING, flags.mode_req_angular_velocity);
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING, flags.mode_req_attitude);
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING, flags.mode_req_local_alt);
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setRequirement(vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING, flags.mode_req_prevent_arming);
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// NAVIGATION_STATE_ACRO
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setRequirement(vehicle_status_s::NAVIGATION_STATE_ACRO, flags.mode_req_angular_velocity);
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setRequirement(vehicle_status_s::NAVIGATION_STATE_ACRO, flags.mode_req_manual_control);
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@@ -540,6 +540,22 @@ PARAM_DEFINE_FLOAT(COM_ARM_AUTH_TO, 1);
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*/
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PARAM_DEFINE_FLOAT(COM_POS_FS_EPH, 5.f);
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/**
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* Loss of position autonomous failsafe action
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*
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* If no autonomous horizontal navigation is possible anymore should the vehicle attempt a dead-reckon
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* return to home or shall it attempt to descend blindly and land.
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*
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* Action to take when autonomous horizontal navigation is lost:
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* - "Dead-Reckon RTH" can be preferred to bring the vehicle back to Line of Sight (LOS) range, at which point the pilot can take over control.
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* - "Land if possible" blind with potential drift and uncontrolled landing (risk of hitting obstacles)
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*
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* @group Commander
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* @value 0 Land if possible
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* @value 1 Dead-Reckoning RTL
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*/
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PARAM_DEFINE_INT32(COM_POS_FS_ACT, 0);
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/**
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* Horizontal velocity error threshold.
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*
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@@ -581,6 +581,16 @@ void FailsafeBase::getSelectedAction(const State &state, const failsafe_flags_s
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returned_state.cause = Cause::Generic;
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// fallthrough
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case Action::DeadReckoningRTL:
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if (modeCanRun(status_flags, vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING)
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&& _param_com_pos_fs_act.get() == 1) {
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selected_action = Action::DeadReckoningRTL;
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break;
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}
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returned_state.cause = Cause::Generic;
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// fallthrough
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case Action::Land:
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if (modeCanRun(status_flags, vehicle_status_s::NAVIGATION_STATE_AUTO_LAND)) {
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@@ -681,6 +691,8 @@ uint8_t FailsafeBase::modeFromAction(const Action &action, uint8_t user_intended
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case Action::RTL: return vehicle_status_s::NAVIGATION_STATE_AUTO_RTL;
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case Action::DeadReckoningRTL: return vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING;
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case Action::Land: return vehicle_status_s::NAVIGATION_STATE_AUTO_LAND;
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case Action::Descend: return vehicle_status_s::NAVIGATION_STATE_DESCEND;
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@@ -61,6 +61,7 @@ public:
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Hold,
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RTL,
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DeadReckoningRTL,
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Land,
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Descend,
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Disarm,
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||||
@@ -105,6 +106,8 @@ public:
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||||
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case Action::RTL: return "RTL";
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case Action::DeadReckoningRTL: return "Dead Reckoning RTL";
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case Action::Land: return "Land";
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case Action::Descend: return "Descend";
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@@ -293,7 +296,8 @@ private:
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void *_on_notify_user_arg{nullptr};
|
||||
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||||
DEFINE_PARAMETERS_CUSTOM_PARENT(ModuleParams,
|
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(ParamFloat<px4::params::COM_FAIL_ACT_T>) _param_com_fail_act_t
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(ParamFloat<px4::params::COM_FAIL_ACT_T>) _param_com_fail_act_t,
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(ParamInt<px4::params::COM_POS_FS_ACT>) _param_com_pos_fs_act
|
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);
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||||
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||||
};
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||||
@@ -73,6 +73,7 @@ enum PX4_CUSTOM_SUB_MODE_AUTO {
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PX4_CUSTOM_SUB_MODE_EXTERNAL6,
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PX4_CUSTOM_SUB_MODE_EXTERNAL7,
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PX4_CUSTOM_SUB_MODE_EXTERNAL8,
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PX4_CUSTOM_SUB_MODE_AUTO_RTL_DR
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};
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enum PX4_CUSTOM_SUB_MODE_POSCTL {
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||||
@@ -226,6 +227,11 @@ static inline union px4_custom_mode get_px4_custom_mode(uint8_t nav_state)
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custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_AUTO;
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custom_mode.sub_mode = PX4_CUSTOM_SUB_MODE_EXTERNAL8;
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break;
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case vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING:
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custom_mode.main_mode = PX4_CUSTOM_MAIN_MODE_AUTO;
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custom_mode.sub_mode = PX4_CUSTOM_SUB_MODE_AUTO_RTL_DR;
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break;
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}
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||||
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return custom_mode;
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@@ -48,6 +48,7 @@ list(APPEND flight_tasks_all
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ManualAltitudeSmoothVel
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ManualPosition
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Transition
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ReturnDeadReckoning
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||||
)
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||||
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||||
if(NOT px4_constrained_flash_build)
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||||
@@ -152,7 +152,10 @@ void FlightModeManager::start_flight_task()
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bool found_some_task = false;
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bool matching_task_running = true;
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bool task_failure = false;
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||||
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const bool nav_state_descend = (_vehicle_status_sub.get().nav_state == vehicle_status_s::NAVIGATION_STATE_DESCEND);
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const bool nav_state_rtl_dr = (_vehicle_status_sub.get().nav_state ==
|
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vehicle_status_s::NAVIGATION_STATE_AUTO_RTL_DEAD_RECKONING);
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||||
|
||||
// Follow me
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if (_vehicle_status_sub.get().nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_FOLLOW_TARGET) {
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@@ -187,7 +190,8 @@ void FlightModeManager::start_flight_task()
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// Navigator interface for autonomous modes
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if (_vehicle_control_mode_sub.get().flag_control_auto_enabled
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&& !nav_state_descend) {
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||||
&& !nav_state_descend
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&& !nav_state_rtl_dr) {
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||||
found_some_task = true;
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||||
|
||||
if (switchTask(FlightTaskIndex::Auto) != FlightTaskError::NoError) {
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||||
@@ -249,6 +253,17 @@ void FlightModeManager::start_flight_task()
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||||
matching_task_running = matching_task_running && !task_failure;
|
||||
}
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||||
|
||||
// Dead-Reckoning Return
|
||||
if (nav_state_rtl_dr) {
|
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found_some_task = true;
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||||
|
||||
FlightTaskError error = switchTask(FlightTaskIndex::ReturnDeadReckoning);
|
||||
|
||||
task_failure = (error != FlightTaskError::NoError);
|
||||
|
||||
matching_task_running = matching_task_running && !task_failure;
|
||||
}
|
||||
|
||||
// Emergency descend
|
||||
if (nav_state_descend || task_failure) {
|
||||
found_some_task = true;
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||||
|
||||
@@ -0,0 +1,39 @@
|
||||
############################################################################
|
||||
#
|
||||
# Copyright (c) 2024 PX4 Development Team. All rights reserved.
|
||||
#
|
||||
# Redistribution and use in source and binary forms, with or without
|
||||
# modification, are permitted provided that the following conditions
|
||||
# are met:
|
||||
#
|
||||
# 1. Redistributions of source code must retain the above copyright
|
||||
# notice, this list of conditions and the following disclaimer.
|
||||
# 2. Redistributions in binary form must reproduce the above copyright
|
||||
# notice, this list of conditions and the following disclaimer in
|
||||
# the documentation and/or other materials provided with the
|
||||
# distribution.
|
||||
# 3. Neither the name PX4 nor the names of its contributors may be
|
||||
# used to endorse or promote products derived from this software
|
||||
# without specific prior written permission.
|
||||
#
|
||||
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
# POSSIBILITY OF SUCH DAMAGE.
|
||||
#
|
||||
############################################################################
|
||||
|
||||
px4_add_library(FlightTaskReturnDeadReckoning
|
||||
FlightTaskReturnDeadReckoning.cpp
|
||||
)
|
||||
|
||||
target_link_libraries(FlightTaskReturnDeadReckoning PUBLIC FlightTask)
|
||||
target_include_directories(FlightTaskReturnDeadReckoning PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
|
||||
+314
@@ -0,0 +1,314 @@
|
||||
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2019-2025 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
/**
|
||||
* @file FlightTaskReturnDeadReckoning.cpp
|
||||
*/
|
||||
|
||||
#include "FlightTaskReturnDeadReckoning.hpp"
|
||||
|
||||
#include <px4_platform_common/events.h>
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::activate(const trajectory_setpoint_s &last_setpoint)
|
||||
{
|
||||
PX4_INFO("FlightTaskReturnDeadReckoning::activate");
|
||||
|
||||
if (!FlightTask::activate(last_setpoint)) {
|
||||
PX4_ERR("Failed to activate task");
|
||||
return false;
|
||||
}
|
||||
|
||||
_updateSubscriptions();
|
||||
_state = State::INIT;
|
||||
|
||||
if (!(_updateBearingToHome() && _initializeSmoothers())) {
|
||||
PX4_ERR("Failed to initialize task");
|
||||
return false;
|
||||
}
|
||||
|
||||
_computeReturnParameters();
|
||||
|
||||
return true;
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::update()
|
||||
{
|
||||
if (!FlightTask::update()) {
|
||||
return false;
|
||||
}
|
||||
|
||||
_updateSubscriptions();
|
||||
|
||||
if (_isGlobalPositionValid()) {
|
||||
// Update the bearing to home if global position is valid
|
||||
if (!_updateBearingToHome()) {
|
||||
PX4_ERR("Failed to compute bearing to home");
|
||||
return false;
|
||||
}
|
||||
}
|
||||
|
||||
_updateState();
|
||||
_updateSetpoints();
|
||||
_updateDistanceFlownEstimate();
|
||||
|
||||
return true;
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_updateState()
|
||||
{
|
||||
switch (_state) {
|
||||
case State::INIT:
|
||||
if (_isAboveReturnAltitude()) {
|
||||
_state = State::RETURN;
|
||||
events::send<float, float>(events::ID("dead_reckon_rtl_return_direct"), events::Log::Info,
|
||||
"Returning to home position to home position at {1:.2m_v} with bearing {2:.2} deg", _rtl_alt,
|
||||
math::degrees(_bearing_to_home));
|
||||
|
||||
} else {
|
||||
_state = State::ASCENT;
|
||||
events::send<float, float>(events::ID("dead_reckon_rtl_ascent"), events::Log::Info,
|
||||
"Ascending to return altitude {1:.2m_v} with bearing {2:.2} deg", _rtl_alt, math::degrees(_bearing_to_home));
|
||||
}
|
||||
|
||||
break;
|
||||
|
||||
case State::ASCENT:
|
||||
if (_isAboveReturnAltitude()) {
|
||||
_state = State::RETURN;
|
||||
events::send<float, float>(events::ID("dead_reckon_rtl_return"), events::Log::Info,
|
||||
"Returning to home position to home position at {1:.2m_v} with bearing {2:.2} deg", _rtl_alt,
|
||||
math::degrees(_bearing_to_home));
|
||||
}
|
||||
|
||||
break;
|
||||
|
||||
case State::RETURN:
|
||||
if (_isReturnComplete()) {
|
||||
_state = State::HOLD;
|
||||
events::send<float>(events::ID("dead_reckon_rtl_hold"), events::Log::Info,
|
||||
"Holding altitude at {1:.2m_v} over home position", _rtl_alt);
|
||||
}
|
||||
|
||||
break;
|
||||
|
||||
case State::HOLD:
|
||||
break;
|
||||
|
||||
default:
|
||||
PX4_ERR("Unknown state");
|
||||
return;
|
||||
}
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_updateSetpoints()
|
||||
{
|
||||
switch (_state) {
|
||||
case State::INIT:
|
||||
_slew_rate_acceleration_x.update(0.0f, _deltatime);
|
||||
_slew_rate_acceleration_y.update(0.0f, _deltatime);
|
||||
_slew_rate_velocity_z.update(0.0f, _deltatime);
|
||||
|
||||
// Hold current altitude
|
||||
_velocity_setpoint(2) = _slew_rate_velocity_z.getState();
|
||||
break;
|
||||
|
||||
case State::ASCENT:
|
||||
_slew_rate_acceleration_x.update(0.0f, _deltatime);
|
||||
_slew_rate_acceleration_y.update(0.0f, _deltatime);
|
||||
_slew_rate_velocity_z.update(-_param_mpc_z_v_auto_up.get(), _deltatime);
|
||||
|
||||
// Ascent until reaching the return altitude
|
||||
_velocity_setpoint(2) = _slew_rate_velocity_z.getState();
|
||||
break;
|
||||
|
||||
case State::RETURN:
|
||||
_slew_rate_acceleration_x.update(_rtl_acc * cosf(_bearing_to_home), _deltatime);
|
||||
_slew_rate_acceleration_y.update(_rtl_acc * sinf(_bearing_to_home), _deltatime);
|
||||
_slew_rate_velocity_z.update(0.0f, _deltatime);
|
||||
|
||||
// Stay at the return altitude
|
||||
_position_setpoint(2) = -(_rtl_alt - (float) _home_position(2));
|
||||
break;
|
||||
|
||||
case State::HOLD:
|
||||
_slew_rate_acceleration_x.update(0.0f, _deltatime);
|
||||
_slew_rate_acceleration_y.update(0.0f, _deltatime);
|
||||
_slew_rate_velocity_z.update(0.0f, _deltatime);
|
||||
|
||||
// Stay at the return altitude
|
||||
_position_setpoint(2) = -(_rtl_alt - (float) _home_position(2));
|
||||
break;
|
||||
|
||||
default:
|
||||
PX4_ERR("Unknown state");
|
||||
return;
|
||||
|
||||
};
|
||||
|
||||
// Heading setpoint
|
||||
_heading_smoothing.update(_bearing_to_home, _deltatime);
|
||||
_yaw_setpoint = _heading_smoothing.getSmoothedHeading();
|
||||
_yawspeed_setpoint = _heading_smoothing.getSmoothedHeadingRate();
|
||||
|
||||
// Acceleration setpoint
|
||||
_acceleration_setpoint.xy() = matrix::Vector2f(
|
||||
_slew_rate_acceleration_x.getState(),
|
||||
_slew_rate_acceleration_y.getState()
|
||||
);
|
||||
|
||||
return;
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_updateDistanceFlownEstimate()
|
||||
{
|
||||
if (_state == State::RETURN) {
|
||||
_distance_flown_estimate += _param_mpc_xy_vel_max.get() * _deltatime;
|
||||
}
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_updateBearingToHome()
|
||||
{
|
||||
if (_readHomePosition(_home_position)) {
|
||||
_readGlobalPosition(_start_vehicle_global_position);
|
||||
_bearing_to_home = _computeBearing(_start_vehicle_global_position, _home_position);
|
||||
|
||||
_distance_flown_estimate = .0f;
|
||||
_initial_distance_to_home = get_distance_to_next_waypoint(
|
||||
_start_vehicle_global_position(0), _start_vehicle_global_position(1),
|
||||
_home_position(0), _home_position(1));
|
||||
}
|
||||
|
||||
return !isnanf(_bearing_to_home);
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_readHomePosition(matrix::Vector3d &home_position)
|
||||
{
|
||||
home_position.setNaN();
|
||||
|
||||
if (_sub_home_position.get().valid_hpos && _sub_home_position.get().valid_alt) {
|
||||
home_position(0) = _sub_home_position.get().lat;
|
||||
home_position(1) = _sub_home_position.get().lon;
|
||||
home_position(2) = (double) _sub_home_position.get().alt;
|
||||
|
||||
return true;
|
||||
}
|
||||
|
||||
return false;
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_readGlobalPosition(matrix::Vector3d &global_position)
|
||||
{
|
||||
|
||||
global_position.setNaN();
|
||||
|
||||
global_position(0) = _sub_vehicle_global_position.get().lat;
|
||||
global_position(1) = _sub_vehicle_global_position.get().lon;
|
||||
global_position(2) = (double) _sub_vehicle_global_position.get().alt;
|
||||
}
|
||||
|
||||
float FlightTaskReturnDeadReckoning::_computeBearing(const matrix::Vector3d &_global_position_start,
|
||||
const matrix::Vector3d &_global_position_end)
|
||||
{
|
||||
float bearing = NAN;
|
||||
|
||||
if (_global_position_start.isAllFinite() && _global_position_end.isAllFinite()) {
|
||||
bearing = get_bearing_to_next_waypoint(_global_position_start(0), _global_position_start(1),
|
||||
_global_position_end(0), _global_position_end(1));
|
||||
}
|
||||
|
||||
return bearing;
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_computeReturnParameters()
|
||||
{
|
||||
_rtl_alt = math::max((float) _start_vehicle_global_position(2),
|
||||
(float) _home_position(2) + _param_rtl_return_alt.get());
|
||||
|
||||
_rtl_acc = _param_mpc_acc_hor_max.get();
|
||||
}
|
||||
|
||||
void FlightTaskReturnDeadReckoning::_updateSubscriptions()
|
||||
{
|
||||
_sub_vehicle_global_position.update();
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_initializeSmoothers()
|
||||
{
|
||||
// Initialize the heading smoother
|
||||
_heading_smoothing.setMaxHeadingRate(_heading_smoothing_scaling_factor * _param_mpc_yawrauto_max.get());
|
||||
_heading_smoothing.setMaxHeadingAccel(_heading_smoothing_scaling_factor * _param_mpc_yawrauto_acc.get());
|
||||
_heading_smoothing.reset(_sub_vehicle_local_position.get().heading, 0.0f);
|
||||
|
||||
// Initialize the position smoother
|
||||
_slew_rate_velocity_z.setSlewRate(_velocity_z_rate_scaling_factor * _param_mpc_acc_up_max.get());
|
||||
_slew_rate_velocity_z.setForcedValue((float) _sub_vehicle_local_position.get().vz);
|
||||
|
||||
// Initialize the acceleration smoothers
|
||||
_slew_rate_acceleration_x.setSlewRate(_jerk_scaling_factor * _param_mpc_jerk_auto.get());
|
||||
_slew_rate_acceleration_x.setForcedValue(_sub_vehicle_local_position.get().ax);
|
||||
_slew_rate_acceleration_y.setSlewRate(_jerk_scaling_factor * _param_mpc_jerk_auto.get());
|
||||
_slew_rate_acceleration_y.setForcedValue(_sub_vehicle_local_position.get().ay);
|
||||
|
||||
return true;
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_isGlobalPositionValid() const
|
||||
{
|
||||
return _sub_vehicle_global_position.get().lat_lon_valid && _sub_vehicle_global_position.get().alt_valid;
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_isAboveReturnAltitude() const
|
||||
{
|
||||
float current_alt = _sub_vehicle_global_position.get().alt;
|
||||
float target_alt = _rtl_alt - _param_nav_mc_alt_rad.get();
|
||||
return current_alt > target_alt;
|
||||
}
|
||||
|
||||
bool FlightTaskReturnDeadReckoning::_isReturnComplete()
|
||||
{
|
||||
bool ret = false;
|
||||
|
||||
if (_isGlobalPositionValid()) {
|
||||
// Close enough to home posititon
|
||||
_readGlobalPosition(_start_vehicle_global_position);
|
||||
ret = get_distance_to_next_waypoint(
|
||||
_start_vehicle_global_position(0), _start_vehicle_global_position(1),
|
||||
_home_position(0), _home_position(1)) < _param_nav_acc_rad.get();
|
||||
}
|
||||
|
||||
if (!ret) {
|
||||
ret = _distance_flown_estimate > 2.5f * _initial_distance_to_home; // 2.5x the initial distance to home
|
||||
}
|
||||
|
||||
return ret;
|
||||
}
|
||||
+172
@@ -0,0 +1,172 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2019-2025 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file FlightTaskReturnDeadReckoning.hpp
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include "FlightTask.hpp"
|
||||
#include <uORB/Subscription.hpp>
|
||||
#include <uORB/topics/vehicle_global_position.h>
|
||||
#include <lib/motion_planning/HeadingSmoothing.hpp>
|
||||
#include <lib/motion_planning/PositionSmoothing.hpp>
|
||||
#include <lib/slew_rate/SlewRate.hpp>
|
||||
|
||||
class FlightTaskReturnDeadReckoning : public FlightTask
|
||||
{
|
||||
public:
|
||||
FlightTaskReturnDeadReckoning() = default;
|
||||
virtual ~FlightTaskReturnDeadReckoning() = default;
|
||||
|
||||
bool activate(const trajectory_setpoint_s &last_setpoint) override;
|
||||
bool update() override;
|
||||
|
||||
private:
|
||||
uORB::SubscriptionData<vehicle_global_position_s> _sub_vehicle_global_position{ORB_ID(vehicle_global_position)};
|
||||
|
||||
/**
|
||||
* Update the flight task state machine
|
||||
*/
|
||||
void _updateState();
|
||||
|
||||
/**
|
||||
* Update the trajectory setpoints according to the current state
|
||||
*/
|
||||
void _updateSetpoints();
|
||||
|
||||
/**
|
||||
* Update estimated flown distance since the last time home bearing was updated
|
||||
*/
|
||||
void _updateDistanceFlownEstimate();
|
||||
|
||||
/**
|
||||
* Update bearing to home position with the last available GNSS position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _updateBearingToHome();
|
||||
|
||||
/**
|
||||
* Initialize home position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _readHomePosition(matrix::Vector3d &home_position);
|
||||
|
||||
/**
|
||||
* Reads current GNSS position
|
||||
*/
|
||||
void _readGlobalPosition(matrix::Vector3d &global_position);
|
||||
|
||||
/**
|
||||
* Compute bearing to home position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
float _computeBearing(const matrix::Vector3d &_global_position_start,
|
||||
const matrix::Vector3d &_global_position_end);
|
||||
|
||||
/**
|
||||
* Computes return altitude and acceleration
|
||||
*/
|
||||
void _computeReturnParameters();
|
||||
|
||||
/**
|
||||
* Update uORB subscriptions
|
||||
*/
|
||||
void _updateSubscriptions();
|
||||
|
||||
/**
|
||||
* Initialize the trajectory setpoint smoothers
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _initializeSmoothers();
|
||||
|
||||
/**
|
||||
* Check if the global position is valid
|
||||
* @return true if valid, false otherwise
|
||||
*/
|
||||
bool _isGlobalPositionValid() const;
|
||||
|
||||
/**
|
||||
* Check if the vehicle is above the return altitude
|
||||
* @return true if above, false otherwise
|
||||
*/
|
||||
bool _isAboveReturnAltitude() const;
|
||||
|
||||
/**
|
||||
* Check if the vehicle is within the home position waypoint acceptance radius, or if the distance traveled is greater than the initial distance to home (times a factor)
|
||||
* @return true if completed, false otherwise
|
||||
*/
|
||||
bool _isReturnComplete();
|
||||
|
||||
|
||||
matrix::Vector3d _home_position; /**< Stores home position */
|
||||
matrix::Vector3d _start_vehicle_global_position; /**< Stores vehicle last known GNSS position */
|
||||
float _bearing_to_home{0.0f}; /**< Stores bearing between home and last GNSS position */
|
||||
float _initial_distance_to_home{0.0f}; /**< Initial distance to home position */
|
||||
float _distance_flown_estimate{0.0f};
|
||||
|
||||
float _heading_smoothing_scaling_factor{0.5f}; /**< Scaling factor applied to heading smoothing limits */
|
||||
HeadingSmoothing _heading_smoothing; /**< Smoother for heading */
|
||||
float _jerk_scaling_factor{0.2f}; /**< Scaling factor applied to acceleration slew rate (jerk) */
|
||||
SlewRate<float> _slew_rate_acceleration_x{0.0f}; /**< Slew rate for x-acceleration setpoint */
|
||||
SlewRate<float> _slew_rate_acceleration_y{0.0f}; /**< Slew rate for y-acceleration setpoint */
|
||||
float _velocity_z_rate_scaling_factor{0.4f}; /**< Scaling factor applied to the vertical velocity slew rate */
|
||||
SlewRate<float> _slew_rate_velocity_z{0.0f}; /**< Slew rate for vertical velocity */
|
||||
|
||||
float _rtl_alt{0.0f}; /**< Return altitude */
|
||||
float _rtl_acc{0.0f}; /**< Return acceleration */
|
||||
|
||||
/**< State machine for flight task */
|
||||
enum class State {
|
||||
UNKNOWN = 0,
|
||||
INIT,
|
||||
ASCENT,
|
||||
RETURN,
|
||||
HOLD
|
||||
};
|
||||
State _state{State::UNKNOWN};
|
||||
|
||||
DEFINE_PARAMETERS_CUSTOM_PARENT(FlightTask,
|
||||
(ParamFloat<px4::params::MPC_ACC_HOR_MAX>) _param_mpc_acc_hor_max,
|
||||
(ParamFloat<px4::params::RTL_RETURN_ALT>) _param_rtl_return_alt, //< RTL altitude
|
||||
(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max, //< max yaw rate in auto modes
|
||||
(ParamFloat<px4::params::MPC_YAWRAUTO_ACC>) _param_mpc_yawrauto_acc, //< max yaw acceleration in auto modes
|
||||
(ParamFloat<px4::params::MPC_JERK_AUTO>) _param_mpc_jerk_auto, //< maximum jerk in auto modes
|
||||
(ParamFloat<px4::params::MPC_Z_V_AUTO_UP>) _param_mpc_z_v_auto_up, //< max vertical velocity up
|
||||
(ParamFloat<px4::params::MPC_ACC_UP_MAX>) _param_mpc_acc_up_max, //< max vertical acceleration up
|
||||
(ParamFloat<px4::params::MPC_XY_VEL_MAX>) _param_mpc_xy_vel_max, //< max horizontal velocity
|
||||
(ParamFloat<px4::params::NAV_MC_ALT_RAD>) _param_nav_mc_alt_rad, //< max vertical error
|
||||
(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad //< max horizontal error
|
||||
);
|
||||
};
|
||||
Reference in New Issue
Block a user