mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-28 12:43:33 +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.
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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
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&& (((now - _state_start_time) > 20_s)
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|| (fabsf(manual_control_setpoint.roll) > 0.05f)
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|| (fabsf(manual_control_setpoint.pitch) > 0.05f))) {
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&& _state != state::idle && should_abort) {
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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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}
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}
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@@ -580,8 +595,7 @@ void McAutotuneAttitudeControl::saveGainsToParams()
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void McAutotuneAttitudeControl::stopAutotune()
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{
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_param_mc_at_start.set(false);
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_param_mc_at_start.commit();
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_vehicle_cmd_start_autotune = false;
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_vehicle_torque_setpoint_sub.unregisterCallback();
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}
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@@ -56,6 +56,7 @@
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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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@@ -86,8 +87,6 @@ public:
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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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@@ -109,6 +108,7 @@ 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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@@ -137,6 +137,9 @@ private:
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int8_t _signal_sign{0};
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bool _armed{false};
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uint8_t _nav_state{0};
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uint8_t _start_flight_mode{0};
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bool _vehicle_cmd_start_autotune{false};
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matrix::Vector3f _kid{};
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matrix::Vector3f _rate_k{};
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@@ -177,7 +180,6 @@ private:
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perf_counter_t _cycle_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": cycle time")};
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DEFINE_PARAMETERS(
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(ParamBool<px4::params::MC_AT_START>) _param_mc_at_start,
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(ParamFloat<px4::params::MC_AT_SYSID_AMP>) _param_mc_at_sysid_amp,
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(ParamInt<px4::params::MC_AT_APPLY>) _param_mc_at_apply,
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(ParamFloat<px4::params::MC_AT_RISE_TIME>) _param_mc_at_rise_time,
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@@ -47,24 +47,6 @@
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*/
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PARAM_DEFINE_INT32(MC_AT_EN, 0);
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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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* Increase the amplitude of the injected signal using
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* MC_AT_SYSID_AMP for more signal/noise ratio
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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(MC_AT_START, 0);
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/**
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* Amplitude of the injected signal
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