mirror of https://github.com/ArduPilot/ardupilot
200 lines
6.2 KiB
C++
200 lines
6.2 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include <AP_HAL/AP_HAL.h>
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#include "AC_PrecLand.h"
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#include "AC_PrecLand_Backend.h"
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#include "AC_PrecLand_Companion.h"
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#include "AC_PrecLand_IRLock.h"
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extern const AP_HAL::HAL& hal;
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const AP_Param::GroupInfo AC_PrecLand::var_info[] = {
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// @Param: ENABLED
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// @DisplayName: Precision Land enabled/disabled and behaviour
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// @Description: Precision Land enabled/disabled and behaviour
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// @Values: 0:Disabled, 1:Enabled Always Land, 2:Enabled Strict
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// @User: Advanced
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AP_GROUPINFO("ENABLED", 0, AC_PrecLand, _enabled, 0),
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// @Param: TYPE
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// @DisplayName: Precision Land Type
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// @Description: Precision Land Type
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// @Values: 0:None, 1:CompanionComputer, 2:IRLock
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// @User: Advanced
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AP_GROUPINFO("TYPE", 1, AC_PrecLand, _type, 0),
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// @Param: SPEED
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// @DisplayName: Precision Land horizontal speed maximum in cm/s
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// @Description: Precision Land horizontal speed maximum in cm/s
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// @Range: 0 500
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// @User: Advanced
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AP_GROUPINFO("SPEED", 2, AC_PrecLand, _speed_xy, AC_PRECLAND_SPEED_XY_DEFAULT),
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// @Param: VEL_P
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// @DisplayName: Precision landing velocity controller P gain
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// @Description: Precision landing velocity controller P gain
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// @Range: 0.100 5.000
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// @User: Advanced
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// @Param: VEL_I
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// @DisplayName: Precision landing velocity controller I gain
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// @Description: Precision landing velocity controller I gain
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// @Range: 0.100 5.000
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// @User: Advanced
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// @Param: VEL_IMAX
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// @DisplayName: Precision landing velocity controller I gain maximum
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// @Description: Precision landing velocity controller I gain maximum
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// @Range: 0 1000
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// @Units: cm/s
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// @User: Standard
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AP_SUBGROUPINFO(_pi_vel_xy, "VEL_", 3, AC_PrecLand, AC_PI_2D),
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AP_GROUPEND
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};
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// Default constructor.
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// Note that the Vector/Matrix constructors already implicitly zero
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// their values.
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//
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AC_PrecLand::AC_PrecLand(const AP_AHRS& ahrs, const AP_InertialNav& inav, float dt) :
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_ahrs(ahrs),
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_inav(inav),
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_pi_vel_xy(PRECLAND_P, PRECLAND_I, PRECLAND_IMAX, PRECLAND_FILT_HZ, dt),
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_dt(dt),
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_have_estimate(false),
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_backend(NULL)
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{
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// set parameters to defaults
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AP_Param::setup_object_defaults(this, var_info);
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// other initialisation
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_backend_state.healthy = false;
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}
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// init - perform any required initialisation of backends
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void AC_PrecLand::init()
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{
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// exit immediately if init has already been run
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if (_backend != NULL) {
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return;
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}
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// default health to false
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_backend = NULL;
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_backend_state.healthy = false;
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// instantiate backend based on type parameter
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switch ((enum PrecLandType)(_type.get())) {
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// no type defined
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case PRECLAND_TYPE_NONE:
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default:
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return;
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// companion computer
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case PRECLAND_TYPE_COMPANION:
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_backend = new AC_PrecLand_Companion(*this, _backend_state);
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break;
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// IR Lock
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#if CONFIG_HAL_BOARD == HAL_BOARD_PX4 || CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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case PRECLAND_TYPE_IRLOCK:
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_backend = new AC_PrecLand_IRLock(*this, _backend_state);
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break;
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#endif
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}
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// init backend
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if (_backend != NULL) {
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_backend->init();
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}
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}
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// update - give chance to driver to get updates from sensor
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void AC_PrecLand::update(float alt_above_terrain_cm)
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{
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// run backend update
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if (_backend != NULL) {
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// read from sensor
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_backend->update();
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// calculate angles to target and position estimate
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calc_angles_and_pos(alt_above_terrain_cm);
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}
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}
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// get_target_shift - returns 3D vector of earth-frame position adjustments to target
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Vector3f AC_PrecLand::get_target_shift(const Vector3f &orig_target)
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{
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Vector3f shift; // default shift initialised to zero
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// do not shift target if not enabled or no position estimate
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if (_backend == NULL || !_have_estimate) {
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return shift;
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}
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// shift is target_offset - (original target - current position)
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Vector3f curr_offset_from_target = orig_target - _inav.get_position();
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shift = _target_pos_offset - curr_offset_from_target;
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shift.z = 0.0f;
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// record we have consumed this reading (perhaps there is a cleaner way to do this using timestamps)
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_have_estimate = false;
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// return adjusted target
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return shift;
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}
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// calc_angles_and_pos - converts sensor's body-frame angles to earth-frame angles and position estimate
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// raw sensor angles stored in _angle_to_target (might be in earth frame, or maybe body frame)
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// earth-frame angles stored in _ef_angle_to_target
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// position estimate is stored in _target_pos
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void AC_PrecLand::calc_angles_and_pos(float alt_above_terrain_cm)
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{
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// exit immediately if not enabled
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if (_backend == NULL) {
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_have_estimate = false;
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return;
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}
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// get angles to target from backend
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if (!_backend->get_angle_to_target(_angle_to_target.x, _angle_to_target.y)) {
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_have_estimate = false;
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return;
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}
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float x_rad;
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float y_rad;
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if(_backend->get_frame_of_reference() == MAV_FRAME_LOCAL_NED){
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//don't subtract vehicle lean angles
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x_rad = _angle_to_target.x;
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y_rad = -_angle_to_target.y;
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}else{ // assume MAV_FRAME_BODY_NED (i.e. a hard-mounted sensor)
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// subtract vehicle lean angles
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x_rad = _angle_to_target.x - _ahrs.roll;
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y_rad = -_angle_to_target.y + _ahrs.pitch;
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}
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// rotate to earth-frame angles
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_ef_angle_to_target.x = y_rad*_ahrs.cos_yaw() - x_rad*_ahrs.sin_yaw();
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_ef_angle_to_target.y = y_rad*_ahrs.sin_yaw() + x_rad*_ahrs.cos_yaw();
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// get current altitude (constrained to no lower than 50cm)
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float alt = MAX(alt_above_terrain_cm, 50.0f);
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// convert earth-frame angles to earth-frame position offset
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_target_pos_offset.x = alt*tanf(_ef_angle_to_target.x);
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_target_pos_offset.y = alt*tanf(_ef_angle_to_target.y);
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_target_pos_offset.z = 0; // not used
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_have_estimate = true;
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}
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// handle_msg - Process a LANDING_TARGET mavlink message
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void AC_PrecLand::handle_msg(mavlink_message_t* msg)
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{
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// run backend update
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if (_backend != NULL) {
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_backend->handle_msg(msg);
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}
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}
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