James Goppert c642025339
vehicle_attitude only based yaw control fix (#10803)
* Add attitude sub to mc_pos_control for yaw usage.

* Initialize pos control _states struct.

* Remove unnecessary init for struct in mc pos ctrl.

* Only use att topic for yaw setting in FlightTask.
2018-11-06 12:03:13 -05:00

145 lines
5.2 KiB
C++

#include "FlightTask.hpp"
#include <mathlib/mathlib.h>
#include <lib/ecl/geo/geo.h>
constexpr uint64_t FlightTask::_timeout;
// First index of empty_setpoint corresponds to time-stamp and requires a finite number.
const vehicle_local_position_setpoint_s FlightTask::empty_setpoint = {0, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, NAN, {NAN, NAN, NAN}};
const vehicle_constraints_s FlightTask::empty_constraints = {0, NAN, NAN, NAN, NAN, NAN, NAN, NAN, vehicle_constraints_s::GEAR_KEEP, {}};
const vehicle_trajectory_waypoint_s FlightTask::empty_trajectory_waypoint = {0, 0, {0, 0, 0, 0, 0, 0, 0},
{ {0, {NAN, NAN, NAN}, {NAN, NAN, NAN}, {NAN, NAN, NAN}, NAN, NAN, false, {0, 0, 0}},
{0, {NAN, NAN, NAN}, {NAN, NAN, NAN}, {NAN, NAN, NAN}, NAN, NAN, false, {0, 0, 0}},
{0, {NAN, NAN, NAN}, {NAN, NAN, NAN}, {NAN, NAN, NAN}, NAN, NAN, false, {0, 0, 0}},
{0, {NAN, NAN, NAN}, {NAN, NAN, NAN}, {NAN, NAN, NAN}, NAN, NAN, false, {0, 0, 0}},
{0, {NAN, NAN, NAN}, {NAN, NAN, NAN}, {NAN, NAN, NAN}, NAN, NAN, false, {0, 0, 0}}
}
};
bool FlightTask::initializeSubscriptions(SubscriptionArray &subscription_array)
{
if (!subscription_array.get(ORB_ID(vehicle_local_position), _sub_vehicle_local_position)) {
return false;
}
if (!subscription_array.get(ORB_ID(vehicle_attitude), _sub_attitude)) {
return false;
}
return true;
}
bool FlightTask::activate()
{
_resetSetpoints();
_setDefaultConstraints();
_time_stamp_activate = hrt_absolute_time();
_heading_reset_counter = _sub_attitude->get().quat_reset_counter;
return true;
}
bool FlightTask::updateInitialize()
{
_time_stamp_current = hrt_absolute_time();
_time = (_time_stamp_current - _time_stamp_activate) / 1e6f;
_deltatime = math::min((_time_stamp_current - _time_stamp_last), _timeout) / 1e6f;
_time_stamp_last = _time_stamp_current;
_evaluateVehicleLocalPosition();
return true;
}
const vehicle_local_position_setpoint_s FlightTask::getPositionSetpoint()
{
/* fill position setpoint message */
vehicle_local_position_setpoint_s vehicle_local_position_setpoint;
vehicle_local_position_setpoint.timestamp = hrt_absolute_time();
vehicle_local_position_setpoint.x = _position_setpoint(0);
vehicle_local_position_setpoint.y = _position_setpoint(1);
vehicle_local_position_setpoint.z = _position_setpoint(2);
vehicle_local_position_setpoint.vx = _velocity_setpoint(0);
vehicle_local_position_setpoint.vy = _velocity_setpoint(1);
vehicle_local_position_setpoint.vz = _velocity_setpoint(2);
vehicle_local_position_setpoint.acc_x = _acceleration_setpoint(0);
vehicle_local_position_setpoint.acc_y = _acceleration_setpoint(1);
vehicle_local_position_setpoint.acc_z = _acceleration_setpoint(2);
_thrust_setpoint.copyTo(vehicle_local_position_setpoint.thrust);
vehicle_local_position_setpoint.yaw = _yaw_setpoint;
vehicle_local_position_setpoint.yawspeed = _yawspeed_setpoint;
return vehicle_local_position_setpoint;
}
void FlightTask::_resetSetpoints()
{
_position_setpoint.setAll(NAN);
_velocity_setpoint.setAll(NAN);
_acceleration_setpoint.setAll(NAN);
_thrust_setpoint.setAll(NAN);
_yaw_setpoint = _yawspeed_setpoint = NAN;
_desired_waypoint = FlightTask::empty_trajectory_waypoint;
}
void FlightTask::_evaluateVehicleLocalPosition()
{
_position.setAll(NAN);
_velocity.setAll(NAN);
_yaw = NAN;
_dist_to_bottom = NAN;
if ((_time_stamp_current - _sub_attitude->get().timestamp) < _timeout) {
// yaw
_yaw = matrix::Eulerf(matrix::Quatf(_sub_attitude->get().q)).psi();
}
// Only use vehicle-local-position topic fields if the topic is received within a certain timestamp
if ((_time_stamp_current - _sub_vehicle_local_position->get().timestamp) < _timeout) {
// position
if (_sub_vehicle_local_position->get().xy_valid) {
_position(0) = _sub_vehicle_local_position->get().x;
_position(1) = _sub_vehicle_local_position->get().y;
}
if (_sub_vehicle_local_position->get().z_valid) {
_position(2) = _sub_vehicle_local_position->get().z;
}
// velocity
if (_sub_vehicle_local_position->get().v_xy_valid) {
_velocity(0) = _sub_vehicle_local_position->get().vx;
_velocity(1) = _sub_vehicle_local_position->get().vy;
}
if (_sub_vehicle_local_position->get().v_z_valid) {
_velocity(2) = _sub_vehicle_local_position->get().vz;
}
// distance to bottom
if (_sub_vehicle_local_position->get().dist_bottom_valid
&& PX4_ISFINITE(_sub_vehicle_local_position->get().dist_bottom)) {
_dist_to_bottom = _sub_vehicle_local_position->get().dist_bottom;
}
// global frame reference coordinates to enable conversions
if (_sub_vehicle_local_position->get().xy_global && _sub_vehicle_local_position->get().z_global) {
globallocalconverter_init(_sub_vehicle_local_position->get().ref_lat, _sub_vehicle_local_position->get().ref_lon,
_sub_vehicle_local_position->get().ref_alt, _sub_vehicle_local_position->get().ref_timestamp);
}
}
}
void FlightTask::_setDefaultConstraints()
{
_constraints.speed_xy = MPC_XY_VEL_MAX.get();
_constraints.speed_up = MPC_Z_VEL_MAX_UP.get();
_constraints.speed_down = MPC_Z_VEL_MAX_DN.get();
_constraints.tilt = math::radians(MPC_TILTMAX_AIR.get());
_constraints.landing_gear = vehicle_constraints_s::GEAR_KEEP;
_constraints.min_distance_to_ground = NAN;
_constraints.max_distance_to_ground = NAN;
}