Files
ardupilot/ArduCopter/mode_circle.cpp
T

144 lines
6.2 KiB
C++

#include "Copter.h"
#include <AP_Mount/AP_Mount.h>
#if MODE_CIRCLE_ENABLED
/*
* Init and run calls for circle flight mode
*/
// circle_init - initialise circle controller flight mode
bool ModeCircle::init(bool ignore_checks)
{
speed_changing = false;
// set speed and acceleration limits
pos_control->NE_set_max_speed_accel_m(wp_nav->get_default_speed_NE_ms(), wp_nav->get_wp_acceleration_mss());
pos_control->NE_set_correction_speed_accel_m(wp_nav->get_default_speed_NE_ms(), wp_nav->get_wp_acceleration_mss());
pos_control->D_set_max_speed_accel_m(get_pilot_speed_dn_ms(), get_pilot_speed_up_ms(), get_pilot_accel_D_mss());
pos_control->D_set_correction_speed_accel_m(get_pilot_speed_dn_ms(), get_pilot_speed_up_ms(), get_pilot_accel_D_mss());
// initialise circle controller including setting the circle center based on vehicle speed
copter.circle_nav->init();
#if HAL_MOUNT_ENABLED
// Check if the CIRCLE_OPTIONS parameter have roi_at_center
if (copter.circle_nav->roi_at_center()) {
const Vector3p &pos_ned_m { copter.circle_nav->get_center_NED_m() };
Location circle_center;
if (!AP::ahrs().get_location_from_origin_offset_NED(circle_center, pos_ned_m)) {
return false;
}
// point at the ground:
circle_center.set_alt_m(0, Location::AltFrame::ABOVE_TERRAIN);
AP_Mount *s = AP_Mount::get_singleton();
s->set_roi_target(circle_center);
}
#endif
// set auto yaw circle mode
auto_yaw.set_mode(AutoYaw::Mode::CIRCLE);
return true;
}
// circle_run - runs the circle flight mode
// should be called at 100hz or more
void ModeCircle::run()
{
// set speed and acceleration limits
pos_control->NE_set_max_speed_accel_m(wp_nav->get_default_speed_NE_ms(), wp_nav->get_wp_acceleration_mss());
pos_control->D_set_max_speed_accel_m(get_pilot_speed_dn_ms(), get_pilot_speed_up_ms(), get_pilot_accel_D_mss());
// Check for any change in params and update in real time
copter.circle_nav->check_param_change();
// pilot changes to circle rate and radius
// skip if in radio failsafe
if (rc().has_valid_input() && copter.circle_nav->pilot_control_enabled()) {
// update the circle controller's radius target based on pilot pitch stick inputs
const float radius_current_m = copter.circle_nav->get_radius_m(); // circle controller's radius target, which begins as the circle_radius parameter
const float pitch_stick_norm = channel_pitch->norm_input_dz(); // pitch stick normalized -1 to 1
const float nav_speed_ms = copter.wp_nav->get_default_speed_NE_ms(); // copter WP_NAV parameter speed
const float radius_pilot_change_m = (pitch_stick_norm * nav_speed_ms) * G_Dt; // rate of change (pitch stick up reduces the radius, as in moving forward)
const float radius_new_m = MAX(radius_current_m + radius_pilot_change_m,0); // new radius target
if (!is_equal(radius_current_m, radius_new_m)) {
copter.circle_nav->set_radius_m(radius_new_m);
}
// update the orbicular rate target based on pilot roll stick inputs
#if AP_RC_TRANSMITTER_TUNING_ENABLED
// skip if using transmitter based tuning knob for circle rate
if (!copter.being_tuned(TUNING_CIRCLE_RATE)) {
#else
{
#endif
const float roll_stick_norm = channel_roll->norm_input_dz(); // roll stick normalized -1 to 1
if (is_zero(roll_stick_norm)) {
// no speed change, so reset speed changing flag
speed_changing = false;
} else {
const float rate_degs = copter.circle_nav->get_rate_degs(); // circle controller's rate target, which begins as the circle_rate parameter
const float rate_target_degs = copter.circle_nav->get_rate_target_degs(); // current adjusted rate target, which is probably different from _rate_degs
const float rate_pilot_change_degs = (roll_stick_norm * G_Dt); // rate of change from 0 to 1 degrees per second
float rate_new_degs = rate_target_degs; // new rate target
if (is_positive(rate_degs)) {
// currently moving clockwise, constrain 0 to 90
rate_new_degs = constrain_float(rate_target_degs + rate_pilot_change_degs, 0, 90);
} else if (is_negative(rate_degs)) {
// currently moving counterclockwise, constrain -90 to 0
rate_new_degs = constrain_float(rate_target_degs + rate_pilot_change_degs, -90, 0);
} else if (is_zero(rate_degs) && !speed_changing) {
// Stopped, pilot has released the roll stick, and pilot now wants to begin moving with the roll stick
rate_new_degs = rate_pilot_change_degs;
}
speed_changing = true;
copter.circle_nav->set_rate_degs(rate_new_degs);
}
}
}
// get pilot desired climb rate (or zero if in radio failsafe)
float target_climb_rate_ms = get_pilot_desired_climb_rate_ms();
// get avoidance adjusted climb rate
target_climb_rate_ms = get_avoidance_adjusted_climbrate_ms(target_climb_rate_ms);
// if not armed set throttle to zero and exit immediately
if (is_disarmed_or_landed()) {
make_safe_ground_handling();
return;
}
// set motors to full range
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
#if AP_RANGEFINDER_ENABLED
// update the vertical offset based on the surface measurement
copter.surface_tracking.update_surface_offset();
#endif
copter.failsafe_terrain_set_status(copter.circle_nav->update_ms(target_climb_rate_ms));
pos_control->D_update_controller();
// call attitude controller with auto yaw
attitude_control->input_thrust_vector_heading(pos_control->get_thrust_vector(), auto_yaw.get_heading());
}
float ModeCircle::wp_distance_m() const
{
return copter.circle_nav->get_distance_to_target_m();
}
float ModeCircle::wp_bearing_deg() const
{
return degrees(copter.circle_nav->get_bearing_to_target_rad());
}
#endif