forked from Archive/PX4-Autopilot
mc_pos_control: refactor spoolup time naming
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@ -159,7 +159,7 @@ private:
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(ParamInt<px4::params::MPC_POS_MODE>) MPC_POS_MODE,
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(ParamInt<px4::params::MPC_AUTO_MODE>) MPC_AUTO_MODE,
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(ParamInt<px4::params::MPC_ALT_MODE>) MPC_ALT_MODE,
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(ParamFloat<px4::params::MPC_IDLE_TKO>) MPC_IDLE_TKO, /**< time constant for smooth takeoff ramp */
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(ParamFloat<px4::params::MPC_SPOOLUP_TIME>) MPC_SPOOLUP_TIME, /**< time to let motors spool up after arming */
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(ParamInt<px4::params::MPC_OBS_AVOID>) MPC_OBS_AVOID, /**< enable obstacle avoidance */
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(ParamFloat<px4::params::MPC_TILTMAX_LND>) MPC_TILTMAX_LND /**< maximum tilt for landing and smooth takeoff */
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);
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@ -185,14 +185,7 @@ private:
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/** During smooth-takeoff, below ALTITUDE_THRESHOLD the yaw-control is turned off ant tilt is limited */
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static constexpr float ALTITUDE_THRESHOLD = 0.3f;
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/**
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* Hysteresis that turns true once vehicle is armed for MPC_IDLE_TKO seconds.
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* A real vehicle requires some time to accelerates the propellers to IDLE speed. To ensure
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* that the propellers reach idle speed before initiating a takeoff, a delay of MPC_IDLE_TKO
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* is added.
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*/
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systemlib::Hysteresis _arm_hysteresis{false}; /**< becomes true once vehicle is armed for MPC_IDLE_TKO seconds */
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systemlib::Hysteresis _spoolup_time_hysteresis{false}; /**< becomes true MPC_SPOOLUP_TIME seconds after the vehicle was armed */
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systemlib::Hysteresis _failsafe_land_hysteresis{false}; /**< becomes true if task did not update correctly for LOITER_TIME_BEFORE_DESCEND */
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WeatherVane *_wv_controller{nullptr};
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@ -411,8 +404,8 @@ MulticopterPositionControl::parameters_update(bool force)
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_tko_speed.set(math::min(_tko_speed.get(), _vel_max_up.get()));
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_land_speed.set(math::min(_land_speed.get(), _vel_max_down.get()));
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// set trigger time for arm hysteresis
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_arm_hysteresis.set_hysteresis_time_from(false, (int)(MPC_IDLE_TKO.get() * (float)1_s));
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// set trigger time for takeoff delay
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_spoolup_time_hysteresis.set_hysteresis_time_from(false, (int)(MPC_SPOOLUP_TIME.get() * (float)1_s));
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if (_wv_controller != nullptr) {
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_wv_controller->update_parameters();
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@ -649,16 +642,15 @@ MulticopterPositionControl::run()
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_wv_controller->update(matrix::Quatf(_att_sp.q_d), _states.yaw);
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}
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// arm hysteresis prevents vehicle to takeoff
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// before propeller reached idle speed.
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_arm_hysteresis.set_state_and_update(_control_mode.flag_armed);
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// start takeoff after delay to allow motors to reach idle speed
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_spoolup_time_hysteresis.set_state_and_update(_control_mode.flag_armed);
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if (_arm_hysteresis.get_state()) {
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// as soon vehicle is armed check for flighttask
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if (_spoolup_time_hysteresis.get_state()) {
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// when vehicle is ready switch to the required flighttask
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start_flight_task();
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} else {
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// disable flighttask
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// stop flighttask while disarmed
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_flight_tasks.switchTask(FlightTaskIndex::None);
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}
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@ -706,9 +698,8 @@ MulticopterPositionControl::run()
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// check if all local states are valid and map accordingly
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set_vehicle_states(setpoint.vz);
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// we can only do a smooth takeoff if a valid velocity or position is available and are
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// armed long enough
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if (_arm_hysteresis.get_state() && PX4_ISFINITE(_states.position(2)) && PX4_ISFINITE(_states.velocity(2))) {
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// do smooth takeoff after delay if there's a valid vertical velocity or position
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if (_spoolup_time_hysteresis.get_state() && PX4_ISFINITE(_states.position(2)) && PX4_ISFINITE(_states.velocity(2))) {
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check_for_smooth_takeoff(setpoint.z, setpoint.vz, constraints);
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update_smooth_takeoff(setpoint.z, setpoint.vz);
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}
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@ -658,7 +658,7 @@ PARAM_DEFINE_FLOAT(MPC_LAND_ALT2, 5.0f);
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PARAM_DEFINE_FLOAT(MPC_TKO_RAMP_T, 0.4f);
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/**
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* Manual-Position control sub-mode.
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* Manual-Position control sub-mode
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*
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* The supported sub-modes are:
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* 0 Default position control where sticks map to position/velocity directly. Maximum speeds
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@ -679,7 +679,7 @@ PARAM_DEFINE_FLOAT(MPC_TKO_RAMP_T, 0.4f);
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PARAM_DEFINE_INT32(MPC_POS_MODE, 1);
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/**
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* Auto sub-mode.
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* Auto sub-mode
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*
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* @value 0 Default line tracking
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* @value 1 Jerk-limited trajectory
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@ -688,20 +688,20 @@ PARAM_DEFINE_INT32(MPC_POS_MODE, 1);
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PARAM_DEFINE_INT32(MPC_AUTO_MODE, 1);
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/**
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* Delay from idle state to arming state.
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* Enforced delay between arming and takeoff
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*
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* For altitude controlled modes, the transition from
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* idle to armed state is delayed by MPC_IDLE_TKO time to ensure
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* that the propellers have reached idle speed before attempting a
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* takeoff. This delay is particularly useful for vehicles with large
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* propellers.
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* For altitude controlled modes the time from arming the motors until
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* a takeoff is possible gets forced to be at least MPC_SPOOLUP_TIME seconds
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* to ensure the motors and propellers can sppol up and reach idle speed before
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* getting commanded to spin faster. This delay is particularly useful for vehicles
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* with slow motor spin-up e.g. because of large propellers.
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*
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* @min 0
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* @max 10
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* @unit sec
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* @unit s
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* @group Multicopter Position Control
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*/
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PARAM_DEFINE_FLOAT(MPC_IDLE_TKO, 0.0f);
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PARAM_DEFINE_FLOAT(MPC_SPOOLUP_TIME, 0.0f);
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/**
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* Flag to enable obstacle avoidance
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@ -713,7 +713,7 @@ PARAM_DEFINE_FLOAT(MPC_IDLE_TKO, 0.0f);
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PARAM_DEFINE_INT32(MPC_OBS_AVOID, 0);
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/**
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* Yaw mode.
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* Yaw mode
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*
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* Specifies the heading in Auto.
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*
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