mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
autotune: enable autotune in mission mode
When operating fully autonomously (i.e., without manual control or a guaranteed link to the ground station), tuning a vehicle can be difficult since the current autotune process requires either RC input or a GCS command. For these scenarios, it it useful to be able to start autotune inside a mission.
This commit is contained in:
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@ -162,6 +162,10 @@ Mission Items:
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- [MAV_CMD_OBLIQUE_SURVEY](https://mavlink.io/en/messages/common.html#MAV_CMD_OBLIQUE_SURVEY)
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- [MAV_CMD_DO_SET_CAMERA_ZOOM](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_SET_CAMERA_ZOOM)
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- [MAV_CMD_DO_SET_CAMERA_FOCUS](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_SET_CAMERA_FOCUS)
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- [MAV_CMD_DO_AUTOTUNE_ENABLE](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_AUTOTUNE_ENABLE)
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- Disabling autotune by setting `param1` to zero is currently not supported. To abort autotune during a mission, switch to another flight mode.
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- Axis selection specified in the MAVLink message is ignored (`param2` must be set to 0).
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Instead, the axis bitmask defined by [`FW_AT_AXES`](../advanced_config/parameter_reference.md#FW_AT_AXES) is used.
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GeoFence Definitions
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@ -166,6 +166,9 @@ Mission Items:
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- [MAV_CMD_NAV_VTOL_TAKEOFF](https://mavlink.io/en/messages/common.html#MAV_CMD_NAV_VTOL_TAKEOFF)
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- `MAV_CMD_NAV_VTOL_TAKEOFF.param2` (transition heading) is ignored.
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Instead the heading to the next waypoint is used for the transition heading. <!-- at LEAST until PX4 v1.13: https://github.com/PX4/PX4-Autopilot/issues/12660 -->
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- [MAV_CMD_DO_AUTOTUNE_ENABLE](https://mavlink.io/en/messages/common.html#MAV_CMD_DO_AUTOTUNE_ENABLE)
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- Disabling autotune by setting `param1` to zero is currently not supported. To abort autotune during a mission, switch to another flight mode.
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- Axis selection specified in the MAVLink message is ignored (`param2` must be set to 0) .
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GeoFence Definitions
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@ -61,6 +61,7 @@ uint16 VEHICLE_CMD_DO_PARACHUTE=208 # Mission command to trigger a parachute. |a
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uint16 VEHICLE_CMD_DO_MOTOR_TEST=209 # Motor test command. |Instance (@range 1, )|throttle type|throttle|timeout [s]|Motor count|Test order|Unused|
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uint16 VEHICLE_CMD_DO_INVERTED_FLIGHT=210 # Change to/from inverted flight. |inverted (0=normal, 1=inverted)|Unused|Unused|Unused|Unused|Unused|Unused|
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uint16 VEHICLE_CMD_DO_GRIPPER = 211 # Command to operate a gripper.
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uint16 VEHICLE_CMD_DO_AUTOTUNE_ENABLE = 212 # Enable autotune module. |1 to enable|Unused|Unused|Unused|Unused|Unused|Unused|
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uint16 VEHICLE_CMD_DO_SET_CAM_TRIGG_INTERVAL=214 # Mission command to set TRIG_INTERVAL for this flight. |[m] Camera trigger distance|Shutter integration time (ms)|Unused|Unused|Unused|Unused|Unused|
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uint16 VEHICLE_CMD_DO_MOUNT_CONTROL_QUAT=220 # Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)|q2 - quaternion param #2, x (0 in null-rotation)|q3 - quaternion param #3, y (0 in null-rotation)|q4 - quaternion param #4, z (0 in null-rotation)|Unused|Unused|Unused|
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uint16 VEHICLE_CMD_DO_GUIDED_MASTER=221 # Set id of master controller. |System ID|Component ID|Unused|Unused|Unused|Unused|Unused|
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@ -1550,6 +1550,7 @@ Commander::handle_command(const vehicle_command_s &cmd)
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case vehicle_command_s::VEHICLE_CMD_EXTERNAL_POSITION_ESTIMATE:
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case vehicle_command_s::VEHICLE_CMD_REQUEST_CAMERA_INFORMATION:
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case vehicle_command_s::VEHICLE_CMD_EXTERNAL_ATTITUDE_ESTIMATE:
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case vehicle_command_s::VEHICLE_CMD_DO_AUTOTUNE_ENABLE:
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/* ignore commands that are handled by other parts of the system */
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break;
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@ -48,7 +48,6 @@ FwAutotuneAttitudeControl::FwAutotuneAttitudeControl(bool is_vtol) :
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_actuator_controls_status_sub(is_vtol ? ORB_ID(actuator_controls_status_1) : ORB_ID(actuator_controls_status_0))
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{
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_autotune_attitude_control_status_pub.advertise();
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reset();
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}
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FwAutotuneAttitudeControl::~FwAutotuneAttitudeControl()
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@ -73,11 +72,6 @@ bool FwAutotuneAttitudeControl::init()
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return true;
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}
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void FwAutotuneAttitudeControl::reset()
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{
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_param_fw_at_start.reset();
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}
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void FwAutotuneAttitudeControl::Run()
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{
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if (should_exit()) {
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@ -107,10 +101,23 @@ void FwAutotuneAttitudeControl::Run()
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}
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}
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if (_vehicle_command_sub.updated()) {
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vehicle_command_s vehicle_command;
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if (_vehicle_command_sub.copy(&vehicle_command)) {
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if (vehicle_command.command == vehicle_command_s::VEHICLE_CMD_DO_AUTOTUNE_ENABLE) {
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if (fabsf(vehicle_command.param1 - 1.0f) < FLT_EPSILON && fabsf(vehicle_command.param2) < FLT_EPSILON) {
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_vehicle_cmd_start_autotune = true;
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}
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}
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}
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}
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_aux_switch_en = isAuxEnableSwitchEnabled();
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_want_start_autotune = _vehicle_cmd_start_autotune || _aux_switch_en;
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// new control data needed every iteration
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if ((_state == state::idle && !_aux_switch_en)
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if ((_state == state::idle && !_want_start_autotune)
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|| !_vehicle_torque_setpoint_sub.updated()) {
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return;
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@ -310,7 +317,8 @@ void FwAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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switch (_state) {
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case state::idle:
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if (_param_fw_at_start.get() || _aux_switch_en) {
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if (_want_start_autotune) {
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mavlink_log_info(&_mavlink_log_pub, "Autotune started");
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_state = state::init;
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@ -540,8 +548,7 @@ void FwAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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orb_advert_t mavlink_log_pub = nullptr;
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mavlink_log_info(&mavlink_log_pub, "Autotune returned to idle");
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_state = state::idle;
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_param_fw_at_start.set(false);
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_param_fw_at_start.commit();
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_vehicle_cmd_start_autotune = false;
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}
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break;
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@ -561,7 +568,7 @@ void FwAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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// Abort
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mavlink_log_critical(&mavlink_log_pub, "Autotune aborted before finishing");
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_state = state::fail;
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_start_flight_mode = _nav_state;
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_state_start_time = now;
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} else if (timeout) {
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@ -589,10 +596,9 @@ void FwAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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break;
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}
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_start_flight_mode = _nav_state;
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_state_start_time = now;
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}
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}
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}
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@ -58,6 +58,7 @@
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#include <uORB/topics/parameter_update.h>
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#include <uORB/topics/autotune_attitude_control_status.h>
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#include <uORB/topics/vehicle_angular_velocity.h>
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#include <uORB/topics/vehicle_command.h>
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/topics/vehicle_torque_setpoint.h>
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#include <mathlib/mathlib.h>
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@ -101,8 +102,6 @@ private:
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void Run() override;
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void reset();
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void checkFilters();
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void updateStateMachine(hrt_abstime now);
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@ -126,6 +125,7 @@ private:
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uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
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uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
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uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
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uORB::Subscription _vehicle_command_sub{ORB_ID(vehicle_command)};
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uORB::PublicationData<autotune_attitude_control_status_s> _autotune_attitude_control_status_pub{ORB_ID(autotune_attitude_control_status)};
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@ -178,6 +178,8 @@ private:
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uint8_t _nav_state{0};
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uint8_t _start_flight_mode{0};
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bool _aux_switch_en{false};
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bool _vehicle_cmd_start_autotune{false};
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bool _want_start_autotune{false};
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orb_advert_t _mavlink_log_pub{nullptr};
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@ -215,7 +217,6 @@ private:
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DEFINE_PARAMETERS(
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(ParamInt<px4::params::FW_AT_AXES>) _param_fw_at_axes,
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(ParamBool<px4::params::FW_AT_START>) _param_fw_at_start,
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(ParamInt<px4::params::FW_AT_MAN_AUX>) _param_fw_at_man_aux,
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(ParamInt<px4::params::FW_AT_APPLY>) _param_fw_at_apply,
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@ -39,22 +39,7 @@
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* @author Mathieu Bresciani <mathieu@auterion.com>
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*/
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/**
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* Start the autotuning sequence
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*
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* WARNING: this will inject steps to the rate controller
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* and can be dangerous. Only activate if you know what you
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* are doing, and in a safe environment.
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*
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* Any motion of the remote stick will abort the signal
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* injection and reset this parameter
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* Best is to perform the identification in position or
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* hold mode.
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*
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* @boolean
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* @group Autotune
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*/
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PARAM_DEFINE_INT32(FW_AT_START, 0);
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/**
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* Controls when to apply the new gains
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@ -1538,6 +1538,12 @@ MavlinkMissionManager::parse_mavlink_mission_item(const mavlink_mission_item_t *
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mission_item->params[0] = (uint16_t)mavlink_mission_item->param1;
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break;
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case MAV_CMD_DO_AUTOTUNE_ENABLE:
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mission_item->nav_cmd = (NAV_CMD)mavlink_mission_item->command;
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mission_item->params[0] = (uint16_t)mavlink_mission_item->param1;
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mission_item->params[1] = (uint16_t)mavlink_mission_item->param2;
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break;
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default:
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mission_item->nav_cmd = NAV_CMD_INVALID;
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PX4_DEBUG("Unsupported command %d", mavlink_mission_item->command);
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@ -1627,6 +1633,7 @@ MavlinkMissionManager::parse_mavlink_mission_item(const mavlink_mission_item_t *
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case MAV_CMD_CONDITION_DELAY:
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case MAV_CMD_CONDITION_DISTANCE:
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case MAV_CMD_DO_SET_ACTUATOR:
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case MAV_CMD_DO_AUTOTUNE_ENABLE:
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case MAV_CMD_COMPONENT_ARM_DISARM:
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mission_item->nav_cmd = (NAV_CMD)mavlink_mission_item->command;
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break;
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@ -622,46 +622,37 @@ void MavlinkReceiver::handle_message_command_both(mavlink_message_t *msg, const
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autotune_attitude_control_status_s status{};
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_autotune_attitude_control_status_sub.copy(&status);
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// if not busy enable via the parameter
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// do not check the return value of the uORB copy above because the module
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// starts publishing only when MC_AT_START is set
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// publish vehicle command once if:
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// - autotune is not already running
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// - we are not in transition
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// - autotune module is enabled
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if (status.state == autotune_attitude_control_status_s::STATE_IDLE) {
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vehicle_status_s vehicle_status{};
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_vehicle_status_sub.copy(&vehicle_status);
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if (!vehicle_status.in_transition_mode) {
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param_t atune_start;
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switch (vehicle_status.vehicle_type) {
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case vehicle_status_s::VEHICLE_TYPE_FIXED_WING:
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atune_start = param_find("FW_AT_START");
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has_module = param_find("FW_AT_APPLY");
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break;
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case vehicle_status_s::VEHICLE_TYPE_ROTARY_WING:
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atune_start = param_find("MC_AT_START");
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has_module = param_find("MC_AT_APPLY");
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break;
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default:
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atune_start = PARAM_INVALID;
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has_module = false;
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break;
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}
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if (atune_start == PARAM_INVALID) {
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has_module = false;
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} else {
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int32_t start = 1;
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param_set(atune_start, &start);
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}
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} else {
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has_module = false;
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}
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}
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if (has_module) {
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_cmd_pub.publish(vehicle_command);
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}
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}
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}
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if (has_module && fabsf(vehicle_command.param1 - 1.f) <= FLT_EPSILON && fabsf(vehicle_command.param2) < FLT_EPSILON) {
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// most are in progress
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result = vehicle_command_ack_s::VEHICLE_CMD_RESULT_IN_PROGRESS;
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@ -715,6 +706,10 @@ void MavlinkReceiver::handle_message_command_both(mavlink_message_t *msg, const
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break;
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}
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} else if (has_module && (fabsf(vehicle_command.param1 - 1.f) > FLT_EPSILON || fabsf(vehicle_command.param2) > FLT_EPSILON)) {
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result = vehicle_command_ack_s::VEHICLE_CMD_RESULT_DENIED;
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} else {
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result = vehicle_command_ack_s::VEHICLE_CMD_RESULT_UNSUPPORTED;
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}
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@ -46,7 +46,6 @@ McAutotuneAttitudeControl::McAutotuneAttitudeControl() :
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WorkItem(MODULE_NAME, px4::wq_configurations::hp_default)
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{
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_autotune_attitude_control_status_pub.advertise();
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reset();
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}
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McAutotuneAttitudeControl::~McAutotuneAttitudeControl()
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@ -56,7 +55,8 @@ McAutotuneAttitudeControl::~McAutotuneAttitudeControl()
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bool McAutotuneAttitudeControl::init()
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{
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if (!_parameter_update_sub.registerCallback()) {
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if (!_vehicle_torque_setpoint_sub.registerCallback()) {
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PX4_ERR("callback registration failed");
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return false;
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}
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@ -66,11 +66,6 @@ bool McAutotuneAttitudeControl::init()
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return true;
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}
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void McAutotuneAttitudeControl::reset()
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{
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_param_mc_at_start.reset();
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}
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void McAutotuneAttitudeControl::Run()
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{
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if (should_exit()) {
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@ -91,17 +86,12 @@ void McAutotuneAttitudeControl::Run()
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updateStateMachine(hrt_absolute_time());
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}
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// new control data needed every iteration
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if (_state == state::idle
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|| !_vehicle_torque_setpoint_sub.updated()) {
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return;
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}
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if (_vehicle_status_sub.updated()) {
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vehicle_status_s vehicle_status;
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if (_vehicle_status_sub.copy(&vehicle_status)) {
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_armed = (vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED);
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_nav_state = vehicle_status.nav_state;
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}
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}
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@ -113,6 +103,24 @@ void McAutotuneAttitudeControl::Run()
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}
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}
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if (_vehicle_command_sub.updated()) {
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vehicle_command_s vehicle_command;
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if (_vehicle_command_sub.copy(&vehicle_command)) {
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if (vehicle_command.command == vehicle_command_s::VEHICLE_CMD_DO_AUTOTUNE_ENABLE) {
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if (fabsf(vehicle_command.param1 - 1.0f) < FLT_EPSILON && fabsf(vehicle_command.param2) < FLT_EPSILON) {
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_vehicle_cmd_start_autotune = true;
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}
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}
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}
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}
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// new control data needed every iteration
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if ((_state == state::idle && !_vehicle_cmd_start_autotune)
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|| !_vehicle_torque_setpoint_sub.updated()) {
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return;
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}
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vehicle_torque_setpoint_s vehicle_torque_setpoint;
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vehicle_angular_velocity_s angular_velocity;
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@ -271,7 +279,7 @@ void McAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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switch (_state) {
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case state::idle:
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if (_param_mc_at_start.get()) {
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if (_vehicle_cmd_start_autotune) {
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if (registerActuatorControlsCallback()) {
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_state = state::init;
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@ -280,6 +288,7 @@ void McAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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}
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_state_start_time = now;
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_start_flight_mode = _nav_state;
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}
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break;
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@ -438,17 +447,23 @@ void McAutotuneAttitudeControl::updateStateMachine(hrt_abstime now)
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break;
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}
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// In case of convergence timeout or pilot intervention,
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// In case of convergence timeout, pilot intervention or mode change,
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// the identification sequence is aborted immediately
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manual_control_setpoint_s manual_control_setpoint{};
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_manual_control_setpoint_sub.copy(&manual_control_setpoint);
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const bool timeout = (now - _state_start_time) > 20_s;
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const bool mode_changed = (_start_flight_mode != _nav_state);
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const bool pilot_intervention = ((fabsf(manual_control_setpoint.roll) > 0.05f)
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|| (fabsf(manual_control_setpoint.pitch) > 0.05f));
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const bool should_abort = timeout || mode_changed || pilot_intervention;
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if (_state != state::wait_for_disarm
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&& _state != state::idle
|
||||
&& (((now - _state_start_time) > 20_s)
|
||||
|| (fabsf(manual_control_setpoint.roll) > 0.05f)
|
||||
|| (fabsf(manual_control_setpoint.pitch) > 0.05f))) {
|
||||
&& _state != state::idle && should_abort) {
|
||||
|
||||
_state = state::fail;
|
||||
_start_flight_mode = _nav_state;
|
||||
_state_start_time = now;
|
||||
}
|
||||
}
|
||||
@ -580,8 +595,7 @@ void McAutotuneAttitudeControl::saveGainsToParams()
|
||||
|
||||
void McAutotuneAttitudeControl::stopAutotune()
|
||||
{
|
||||
_param_mc_at_start.set(false);
|
||||
_param_mc_at_start.commit();
|
||||
_vehicle_cmd_start_autotune = false;
|
||||
_vehicle_torque_setpoint_sub.unregisterCallback();
|
||||
}
|
||||
|
||||
|
||||
@ -56,6 +56,7 @@
|
||||
#include <uORB/topics/parameter_update.h>
|
||||
#include <uORB/topics/autotune_attitude_control_status.h>
|
||||
#include <uORB/topics/vehicle_angular_velocity.h>
|
||||
#include <uORB/topics/vehicle_command.h>
|
||||
#include <uORB/topics/vehicle_status.h>
|
||||
#include <uORB/topics/vehicle_torque_setpoint.h>
|
||||
#include <mathlib/mathlib.h>
|
||||
@ -86,8 +87,6 @@ public:
|
||||
private:
|
||||
void Run() override;
|
||||
|
||||
void reset();
|
||||
|
||||
void checkFilters();
|
||||
|
||||
void updateStateMachine(hrt_abstime now);
|
||||
@ -109,6 +108,7 @@ private:
|
||||
uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
|
||||
uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
|
||||
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
|
||||
uORB::Subscription _vehicle_command_sub{ORB_ID(vehicle_command)};
|
||||
|
||||
uORB::PublicationData<autotune_attitude_control_status_s> _autotune_attitude_control_status_pub{ORB_ID(autotune_attitude_control_status)};
|
||||
|
||||
@ -137,6 +137,9 @@ private:
|
||||
int8_t _signal_sign{0};
|
||||
|
||||
bool _armed{false};
|
||||
uint8_t _nav_state{0};
|
||||
uint8_t _start_flight_mode{0};
|
||||
bool _vehicle_cmd_start_autotune{false};
|
||||
|
||||
matrix::Vector3f _kid{};
|
||||
matrix::Vector3f _rate_k{};
|
||||
@ -177,7 +180,6 @@ private:
|
||||
perf_counter_t _cycle_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": cycle time")};
|
||||
|
||||
DEFINE_PARAMETERS(
|
||||
(ParamBool<px4::params::MC_AT_START>) _param_mc_at_start,
|
||||
(ParamFloat<px4::params::MC_AT_SYSID_AMP>) _param_mc_at_sysid_amp,
|
||||
(ParamInt<px4::params::MC_AT_APPLY>) _param_mc_at_apply,
|
||||
(ParamFloat<px4::params::MC_AT_RISE_TIME>) _param_mc_at_rise_time,
|
||||
|
||||
@ -47,24 +47,6 @@
|
||||
*/
|
||||
PARAM_DEFINE_INT32(MC_AT_EN, 0);
|
||||
|
||||
/**
|
||||
* Start the autotuning sequence
|
||||
*
|
||||
* WARNING: this will inject steps to the rate controller
|
||||
* and can be dangerous. Only activate if you know what you
|
||||
* are doing, and in a safe environment.
|
||||
*
|
||||
* Any motion of the remote stick will abort the signal
|
||||
* injection and reset this parameter
|
||||
* Best is to perform the identification in position or
|
||||
* hold mode.
|
||||
* Increase the amplitude of the injected signal using
|
||||
* MC_AT_SYSID_AMP for more signal/noise ratio
|
||||
*
|
||||
* @boolean
|
||||
* @group Autotune
|
||||
*/
|
||||
PARAM_DEFINE_INT32(MC_AT_START, 0);
|
||||
|
||||
/**
|
||||
* Amplitude of the injected signal
|
||||
|
||||
@ -257,6 +257,7 @@ bool FeasibilityChecker::checkMissionItemValidity(mission_item_s &mission_item,
|
||||
mission_item.nav_cmd != NAV_CMD_CONDITION_GATE &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_WINCH &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_GRIPPER &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_AUTOTUNE_ENABLE &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_JUMP &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_CHANGE_SPEED &&
|
||||
mission_item.nav_cmd != NAV_CMD_DO_SET_HOME &&
|
||||
|
||||
@ -83,6 +83,7 @@ MissionBlock::is_mission_item_reached_or_completed()
|
||||
case NAV_CMD_DO_MOUNT_CONTROL:
|
||||
case NAV_CMD_DO_GIMBAL_MANAGER_CONFIGURE:
|
||||
case NAV_CMD_COMPONENT_ARM_DISARM:
|
||||
case NAV_CMD_DO_AUTOTUNE_ENABLE:
|
||||
case NAV_CMD_DO_SET_ROI:
|
||||
case NAV_CMD_DO_SET_ROI_LOCATION:
|
||||
case NAV_CMD_DO_SET_ROI_WPNEXT_OFFSET:
|
||||
|
||||
@ -73,6 +73,7 @@ enum NAV_CMD {
|
||||
NAV_CMD_DO_MOUNT_CONFIGURE = 204,
|
||||
NAV_CMD_DO_MOUNT_CONTROL = 205,
|
||||
NAV_CMD_DO_GRIPPER = 211,
|
||||
NAV_CMD_DO_AUTOTUNE_ENABLE = 212,
|
||||
NAV_CMD_DO_SET_CAM_TRIGG_INTERVAL = 214,
|
||||
NAV_CMD_DO_SET_CAM_TRIGG_DIST = 206,
|
||||
NAV_CMD_OBLIQUE_SURVEY = 260,
|
||||
|
||||
@ -759,6 +759,21 @@ void Navigator::run()
|
||||
reset_cruising_speed();
|
||||
set_cruising_throttle();
|
||||
}
|
||||
|
||||
else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_AUTOTUNE_ENABLE) {
|
||||
|
||||
|
||||
if (fabsf(cmd.param1 - 1.f) > FLT_EPSILON) {
|
||||
// only support enabling autotune (consistent with autotune module)
|
||||
events::send(events::ID("navigator_autotune_unsupported_input"), {events::Log::Warning, events::LogInternal::Warning},
|
||||
"Provided autotune command is not supported. To enable autotune in mission, set param1 to 1");
|
||||
|
||||
} else if (fabsf(cmd.param2) > FLT_EPSILON) {
|
||||
// warn user about axis selection
|
||||
events::send(events::ID("navigator_autotune_unsupported_ax"), {events::Log::Warning, events::LogInternal::Info},
|
||||
"Autotune axis selection not supported through Mission. Use FW_AT_AXES to set axes for fixed-wing vehicles");
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
#if CONFIG_NAVIGATOR_ADSB
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user