2017-11-08 10:57:56 +01:00
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#include "FlightTask.hpp"
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#include <mathlib/mathlib.h>
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2017-11-08 22:31:14 +01:00
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constexpr uint64_t FlightTask::_timeout;
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2018-04-26 11:21:26 +02:00
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// First index of empty_setpoint corresponds to time-stamp and requires a finite number.
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2018-02-06 18:14:08 +01:00
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const vehicle_local_position_setpoint_s FlightTask::empty_setpoint = {0, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, {NAN, NAN, NAN}};
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2018-04-26 11:21:26 +02:00
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const vehicle_constraints_s FlightTask::empty_constraints = {0, NAN, NAN, NAN};
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2017-11-20 21:55:28 +01:00
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bool FlightTask::initializeSubscriptions(SubscriptionArray &subscription_array)
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{
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if (!subscription_array.get(ORB_ID(vehicle_local_position), _sub_vehicle_local_position)) {
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return false;
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}
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return true;
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}
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2017-11-28 22:00:46 +01:00
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bool FlightTask::activate()
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2017-11-27 21:31:47 +01:00
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{
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2018-02-28 09:30:20 +01:00
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_resetSetpoints();
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2018-04-26 11:22:18 +02:00
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_setDefaultConstraints();
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2017-11-27 21:31:47 +01:00
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_time_stamp_activate = hrt_absolute_time();
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2017-11-28 22:00:46 +01:00
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return true;
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2017-11-27 21:31:47 +01:00
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}
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2017-11-28 22:00:46 +01:00
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bool FlightTask::updateInitialize()
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2017-11-08 10:57:56 +01:00
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{
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2017-11-20 14:27:56 +01:00
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_time_stamp_current = hrt_absolute_time();
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_time = (_time_stamp_current - _time_stamp_activate) / 1e6f;
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_deltatime = math::min((_time_stamp_current - _time_stamp_last), _timeout) / 1e6f;
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_time_stamp_last = _time_stamp_current;
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2018-03-09 08:18:36 +01:00
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return _evaluateVehicleLocalPosition();
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2017-11-08 10:57:56 +01:00
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}
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2018-02-28 09:30:20 +01:00
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const vehicle_local_position_setpoint_s FlightTask::getPositionSetpoint()
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{
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/* fill position setpoint message */
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vehicle_local_position_setpoint_s vehicle_local_position_setpoint;
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vehicle_local_position_setpoint.timestamp = hrt_absolute_time();
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_position_setpoint.copyToRaw(&vehicle_local_position_setpoint.x);
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_velocity_setpoint.copyToRaw(&vehicle_local_position_setpoint.vx);
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_acceleration_setpoint.copyToRaw(&vehicle_local_position_setpoint.acc_x);
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_thrust_setpoint.copyTo(vehicle_local_position_setpoint.thrust);
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vehicle_local_position_setpoint.yaw = _yaw_setpoint;
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vehicle_local_position_setpoint.yawspeed = _yawspeed_setpoint;
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return vehicle_local_position_setpoint;
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}
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void FlightTask::_resetSetpoints()
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{
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_position_setpoint *= NAN;
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_velocity_setpoint *= NAN;
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_acceleration_setpoint *= NAN;
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_thrust_setpoint *= NAN;
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_yaw_setpoint = _yawspeed_setpoint = NAN;
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}
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2018-03-09 08:18:36 +01:00
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bool FlightTask::_evaluateVehicleLocalPosition()
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2017-11-08 10:57:56 +01:00
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{
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2017-11-20 21:55:28 +01:00
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if ((_time_stamp_current - _sub_vehicle_local_position->get().timestamp) < _timeout) {
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2018-05-24 08:49:18 +02:00
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// position
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if (_sub_vehicle_local_position->get().xy_valid) {
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_position(0) = _sub_vehicle_local_position->get().x;
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_position(1) = _sub_vehicle_local_position->get().y;
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} else {
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_position(0) = _position(1) = NAN;
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}
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if (_sub_vehicle_local_position->get().z_valid) {
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_position(2) = _sub_vehicle_local_position->get().z;
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} else {
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_position(2) = NAN;
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}
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// velocity
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if (_sub_vehicle_local_position->get().v_xy_valid) {
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_velocity(0) = _sub_vehicle_local_position->get().vx;
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_velocity(1) = _sub_vehicle_local_position->get().vy;
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} else {
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_velocity(0) = _velocity(1) = NAN;
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}
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if (_sub_vehicle_local_position->get().v_z_valid) {
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_velocity(2) = _sub_vehicle_local_position->get().vz;
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} else {
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_velocity(2) = NAN;
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}
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// yaw
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2017-11-20 21:55:28 +01:00
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_yaw = _sub_vehicle_local_position->get().yaw;
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2018-05-24 08:49:18 +02:00
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2018-06-21 20:05:10 +02:00
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// distance to bottom
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2018-04-18 11:17:53 +02:00
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_dist_to_bottom = NAN;
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if (_sub_vehicle_local_position->get().dist_bottom_valid) {
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_dist_to_bottom = _sub_vehicle_local_position->get().dist_bottom;
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}
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2018-06-21 20:05:10 +02:00
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// estimator specified vehicle limits
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2018-05-24 08:49:18 +02:00
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// We don't check here if states are valid or not.
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// Validity checks are done in the sub-classes.
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2017-11-28 22:00:46 +01:00
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return true;
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2017-11-08 10:57:56 +01:00
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} else {
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2018-04-18 11:21:36 +02:00
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_resetSetpoints();
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2017-11-28 22:00:46 +01:00
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return false;
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2017-11-08 10:57:56 +01:00
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}
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}
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2018-04-18 11:20:51 +02:00
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2018-04-26 11:22:18 +02:00
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void FlightTask::_setDefaultConstraints()
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2018-04-18 11:20:51 +02:00
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{
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2018-04-26 11:22:18 +02:00
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_constraints.speed_xy = MPC_XY_VEL_MAX.get();
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_constraints.speed_up = MPC_Z_VEL_MAX_UP.get();
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_constraints.speed_down = MPC_Z_VEL_MAX_DN.get();
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_constraints.tilt = math::radians(MPC_TILTMAX_AIR.get());
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2018-04-27 10:38:25 +02:00
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_constraints.landing_gear = vehicle_constraints_s::GEAR_KEEP;
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2018-05-24 17:59:48 +02:00
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_constraints.min_distance_to_ground = NAN;
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2018-04-18 11:20:51 +02:00
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}
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