mirror of https://github.com/ArduPilot/ardupilot
382 lines
13 KiB
C++
382 lines
13 KiB
C++
#include <AP_HAL/AP_HAL.h>
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#include <AP_Math/AP_Math.h>
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#include <AP_Terrain/AP_Terrain.h>
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#include "AC_Circle.h"
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#include <AP_Logger/AP_Logger.h>
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extern const AP_HAL::HAL& hal;
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const AP_Param::GroupInfo AC_Circle::var_info[] = {
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// @Param: RADIUS
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// @DisplayName: Circle Radius
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// @Description: Defines the radius of the circle the vehicle will fly when in Circle flight mode
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// @Units: cm
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// @Range: 0 200000
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// @Increment: 100
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// @User: Standard
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AP_GROUPINFO("RADIUS", 0, AC_Circle, _radius_parm, AC_CIRCLE_RADIUS_DEFAULT),
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// @Param: RATE
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// @DisplayName: Circle rate
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// @Description: Circle mode's turn rate in deg/sec. Positive to turn clockwise, negative for counter clockwise. Circle rate must be less than ATC_SLEW_YAW parameter.
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// @Units: deg/s
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// @Range: -90 90
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// @Increment: 1
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// @User: Standard
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AP_GROUPINFO("RATE", 1, AC_Circle, _rate_parm, AC_CIRCLE_RATE_DEFAULT),
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// @Param: OPTIONS
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// @DisplayName: Circle options
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// @Description: 0:Enable or disable using the pitch/roll stick control circle mode's radius and rate
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// @Bitmask: 0:manual control, 1:face direction of travel, 2:Start at center rather than on perimeter, 3:Make Mount ROI the center of the circle
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// @User: Standard
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AP_GROUPINFO("OPTIONS", 2, AC_Circle, _options, 1),
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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_Circle::AC_Circle(const AP_InertialNav& inav, const AP_AHRS_View& ahrs, AC_PosControl& pos_control) :
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_inav(inav),
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_ahrs(ahrs),
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_pos_control(pos_control)
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{
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AP_Param::setup_object_defaults(this, var_info);
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// init flags
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_flags.panorama = false;
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_rate = _rate_parm;
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}
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/// init - initialise circle controller setting center specifically
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/// set terrain_alt to true if center.z should be interpreted as an alt-above-terrain. Rate should be +ve in deg/sec for cw turn
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/// caller should set the position controller's x,y and z speeds and accelerations before calling this
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void AC_Circle::init(const Vector3p& center, bool terrain_alt, float rate_deg_per_sec)
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{
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_center = center;
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_terrain_alt = terrain_alt;
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_rate = rate_deg_per_sec;
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// initialise position controller (sets target roll angle, pitch angle and I terms based on vehicle current lean angles)
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_pos_control.init_xy_controller_stopping_point();
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_pos_control.init_z_controller_stopping_point();
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// calculate velocities
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calc_velocities(true);
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// set start angle from position
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init_start_angle(false);
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}
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/// init - initialise circle controller setting center using stopping point and projecting out based on the copter's heading
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/// caller should set the position controller's x,y and z speeds and accelerations before calling this
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void AC_Circle::init()
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{
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// initialize radius and rate from params
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_radius = _radius_parm;
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_last_radius_param = _radius_parm;
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_rate = _rate_parm;
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// initialise position controller (sets target roll angle, pitch angle and I terms based on vehicle current lean angles)
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_pos_control.init_xy_controller_stopping_point();
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_pos_control.init_z_controller_stopping_point();
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// get stopping point
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const Vector3p& stopping_point = _pos_control.get_pos_target_cm();
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// set circle center to circle_radius ahead of stopping point
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_center = stopping_point;
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if ((_options.get() & CircleOptions::INIT_AT_CENTER) == 0) {
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_center.x += _radius * _ahrs.cos_yaw();
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_center.y += _radius * _ahrs.sin_yaw();
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}
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_terrain_alt = false;
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// calculate velocities
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calc_velocities(true);
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// set starting angle from vehicle heading
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init_start_angle(true);
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}
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/// set circle center to a Location
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void AC_Circle::set_center(const Location& center)
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{
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if (center.get_alt_frame() == Location::AltFrame::ABOVE_TERRAIN) {
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// convert Location with terrain altitude
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Vector2f center_xy;
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int32_t terr_alt_cm;
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if (center.get_vector_xy_from_origin_NE(center_xy) && center.get_alt_cm(Location::AltFrame::ABOVE_TERRAIN, terr_alt_cm)) {
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set_center(Vector3f(center_xy.x, center_xy.y, terr_alt_cm), true);
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} else {
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// failed to convert location so set to current position and log error
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set_center(_inav.get_position_neu_cm(), false);
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LOGGER_WRITE_ERROR(LogErrorSubsystem::NAVIGATION, LogErrorCode::FAILED_CIRCLE_INIT);
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}
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} else {
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// convert Location with alt-above-home, alt-above-origin or absolute alt
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Vector3f circle_center_neu;
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if (!center.get_vector_from_origin_NEU(circle_center_neu)) {
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// default to current position and log error
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circle_center_neu = _inav.get_position_neu_cm();
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LOGGER_WRITE_ERROR(LogErrorSubsystem::NAVIGATION, LogErrorCode::FAILED_CIRCLE_INIT);
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}
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set_center(circle_center_neu, false);
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}
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}
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/// set_circle_rate - set circle rate in degrees per second
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void AC_Circle::set_rate(float deg_per_sec)
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{
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if (!is_equal(deg_per_sec, _rate)) {
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_rate = deg_per_sec;
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}
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}
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/// set_circle_rate - set circle rate in degrees per second
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void AC_Circle::set_radius_cm(float radius_cm)
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{
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_radius = constrain_float(radius_cm, 0, AC_CIRCLE_RADIUS_MAX);
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}
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/// returns true if update has been run recently
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/// used by vehicle code to determine if get_yaw() is valid
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bool AC_Circle::is_active() const
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{
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return (AP_HAL::millis() - _last_update_ms < 200);
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}
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/// update - update circle controller
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bool AC_Circle::update(float climb_rate_cms)
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{
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calc_velocities(false);
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// calculate dt
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const float dt = _pos_control.get_dt();
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// ramp angular velocity to maximum
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if (_angular_vel < _angular_vel_max) {
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_angular_vel += fabsf(_angular_accel) * dt;
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_angular_vel = MIN(_angular_vel, _angular_vel_max);
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}
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if (_angular_vel > _angular_vel_max) {
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_angular_vel -= fabsf(_angular_accel) * dt;
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_angular_vel = MAX(_angular_vel, _angular_vel_max);
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}
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// update the target angle and total angle travelled
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float angle_change = _angular_vel * dt;
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_angle += angle_change;
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_angle = wrap_PI(_angle);
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_angle_total += angle_change;
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// calculate terrain adjustments
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float terr_offset = 0.0f;
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if (_terrain_alt && !get_terrain_offset(terr_offset)) {
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return false;
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}
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// calculate z-axis target
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float target_z_cm;
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if (_terrain_alt) {
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target_z_cm = _center.z + terr_offset;
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} else {
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target_z_cm = _pos_control.get_pos_target_z_cm();
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}
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// if the circle_radius is zero we are doing panorama so no need to update loiter target
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Vector3p target {
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_center.x,
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_center.y,
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target_z_cm
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};
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if (!is_zero(_radius)) {
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// calculate target position
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target.x += _radius * cosf(-_angle);
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target.y += - _radius * sinf(-_angle);
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// heading is from vehicle to center of circle
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_yaw = get_bearing_cd(_inav.get_position_xy_cm(), _center.tofloat().xy());
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if ((_options.get() & CircleOptions::FACE_DIRECTION_OF_TRAVEL) != 0) {
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_yaw += is_positive(_rate)?-9000.0f:9000.0f;
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_yaw = wrap_360_cd(_yaw);
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}
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} else {
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// heading is same as _angle but converted to centi-degrees
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_yaw = _angle * DEGX100;
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}
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// update position controller target
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Vector2f zero;
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_pos_control.input_pos_vel_accel_xy(target.xy(), zero, zero);
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if (_terrain_alt) {
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float zero2 = 0;
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float target_zf = target.z;
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_pos_control.input_pos_vel_accel_z(target_zf, zero2, 0);
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} else {
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_pos_control.set_pos_target_z_from_climb_rate_cm(climb_rate_cms);
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}
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// update position controller
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_pos_control.update_xy_controller();
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// set update time
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_last_update_ms = AP_HAL::millis();
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return true;
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}
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// get_closest_point_on_circle - returns closest point on the circle
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// circle's center should already have been set
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// closest point on the circle will be placed in result
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// result's altitude (i.e. z) will be set to the circle_center's altitude
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// if vehicle is at the center of the circle, the edge directly behind vehicle will be returned
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void AC_Circle::get_closest_point_on_circle(Vector3f &result) const
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{
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// return center if radius is zero
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if (_radius <= 0) {
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result = _center.tofloat();
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return;
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}
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// get current position
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Vector2p stopping_point;
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_pos_control.get_stopping_point_xy_cm(stopping_point);
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// calc vector from stopping point to circle center
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Vector2f vec = (stopping_point - _center.xy()).tofloat();
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float dist = vec.length();
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// if current location is exactly at the center of the circle return edge directly behind vehicle
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if (is_zero(dist)) {
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result.x = _center.x - _radius * _ahrs.cos_yaw();
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result.y = _center.y - _radius * _ahrs.sin_yaw();
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result.z = _center.z;
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return;
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}
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// calculate closest point on edge of circle
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result.x = _center.x + vec.x / dist * _radius;
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result.y = _center.y + vec.y / dist * _radius;
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result.z = _center.z;
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}
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// calc_velocities - calculate angular velocity max and acceleration based on radius and rate
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// this should be called whenever the radius or rate are changed
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// initialises the yaw and current position around the circle
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void AC_Circle::calc_velocities(bool init_velocity)
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{
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// if we are doing a panorama set the circle_angle to the current heading
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if (_radius <= 0) {
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_angular_vel_max = ToRad(_rate);
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_angular_accel = MAX(fabsf(_angular_vel_max),ToRad(AC_CIRCLE_ANGULAR_ACCEL_MIN)); // reach maximum yaw velocity in 1 second
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}else{
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// calculate max velocity based on waypoint speed ensuring we do not use more than half our max acceleration for accelerating towards the center of the circle
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float velocity_max = MIN(_pos_control.get_max_speed_xy_cms(), safe_sqrt(0.5f*_pos_control.get_max_accel_xy_cmss()*_radius));
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// angular_velocity in radians per second
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_angular_vel_max = velocity_max/_radius;
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_angular_vel_max = constrain_float(ToRad(_rate),-_angular_vel_max,_angular_vel_max);
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// angular_velocity in radians per second
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_angular_accel = MAX(_pos_control.get_max_accel_xy_cmss()/_radius, ToRad(AC_CIRCLE_ANGULAR_ACCEL_MIN));
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}
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// initialise angular velocity
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if (init_velocity) {
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_angular_vel = 0;
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}
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}
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// init_start_angle - sets the starting angle around the circle and initialises the angle_total
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// if use_heading is true the vehicle's heading will be used to init the angle causing minimum yaw movement
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// if use_heading is false the vehicle's position from the center will be used to initialise the angle
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void AC_Circle::init_start_angle(bool use_heading)
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{
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// initialise angle total
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_angle_total = 0;
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// if the radius is zero we are doing panorama so init angle to the current heading
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if (_radius <= 0) {
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_angle = _ahrs.yaw;
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return;
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}
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// if use_heading is true
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if (use_heading) {
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_angle = wrap_PI(_ahrs.yaw-M_PI);
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} else {
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// if we are exactly at the center of the circle, init angle to directly behind vehicle (so vehicle will backup but not change heading)
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const Vector3f &curr_pos = _inav.get_position_neu_cm();
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if (is_equal(curr_pos.x,float(_center.x)) && is_equal(curr_pos.y,float(_center.y))) {
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_angle = wrap_PI(_ahrs.yaw-M_PI);
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} else {
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// get bearing from circle center to vehicle in radians
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float bearing_rad = atan2f(curr_pos.y-_center.y,curr_pos.x-_center.x);
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_angle = wrap_PI(bearing_rad);
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}
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}
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}
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// get expected source of terrain data
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AC_Circle::TerrainSource AC_Circle::get_terrain_source() const
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{
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// use range finder if connected
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if (_rangefinder_available) {
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return AC_Circle::TerrainSource::TERRAIN_FROM_RANGEFINDER;
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}
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#if AP_TERRAIN_AVAILABLE
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const AP_Terrain *terrain = AP_Terrain::get_singleton();
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if ((terrain != nullptr) && terrain->enabled()) {
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return AC_Circle::TerrainSource::TERRAIN_FROM_TERRAINDATABASE;
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} else {
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return AC_Circle::TerrainSource::TERRAIN_UNAVAILABLE;
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}
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#else
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return AC_Circle::TerrainSource::TERRAIN_UNAVAILABLE;
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#endif
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}
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// get terrain's altitude (in cm above the ekf origin) at the current position (+ve means terrain below vehicle is above ekf origin's altitude)
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bool AC_Circle::get_terrain_offset(float& offset_cm)
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{
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// calculate offset based on source (rangefinder or terrain database)
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switch (get_terrain_source()) {
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case AC_Circle::TerrainSource::TERRAIN_UNAVAILABLE:
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return false;
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case AC_Circle::TerrainSource::TERRAIN_FROM_RANGEFINDER:
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if (_rangefinder_healthy) {
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offset_cm = _rangefinder_terrain_offset_cm;
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return true;
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}
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return false;
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case AC_Circle::TerrainSource::TERRAIN_FROM_TERRAINDATABASE:
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#if AP_TERRAIN_AVAILABLE
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float terr_alt = 0.0f;
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AP_Terrain *terrain = AP_Terrain::get_singleton();
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if (terrain != nullptr && terrain->height_above_terrain(terr_alt, true)) {
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offset_cm = _inav.get_position_z_up_cm() - (terr_alt * 100.0);
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return true;
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}
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#endif
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return false;
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}
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// we should never get here but just in case
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return false;
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}
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void AC_Circle::check_param_change()
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{
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if (!is_equal(_last_radius_param,_radius_parm.get())) {
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_radius = _radius_parm;
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_last_radius_param = _radius_parm;
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}
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}
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