ardupilot/ArduCopter/control_circle.pde

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
* control_circle.pde - init and run calls for circle flight mode
*/
// circle_init - initialise circle controller flight mode
static bool circle_init(bool ignore_checks)
{
if (position_ok() || ignore_checks) {
circle_pilot_yaw_override = false;
// initialize speeds and accelerations
pos_control.set_speed_xy(wp_nav.get_speed_xy());
pos_control.set_accel_xy(wp_nav.get_wp_acceleration());
pos_control.set_speed_z(-g.pilot_velocity_z_max, g.pilot_velocity_z_max);
pos_control.set_accel_z(g.pilot_accel_z);
// initialise circle controller including setting the circle center based on vehicle speed
circle_nav.init();
return true;
}else{
return false;
}
}
// circle_run - runs the circle flight mode
// should be called at 100hz or more
static void circle_run()
{
float target_yaw_rate = 0;
float target_climb_rate = 0;
// if not auto armed set throttle to zero and exit immediately
if(!ap.auto_armed || ap.land_complete) {
// To-Do: add some initialisation of position controllers
attitude_control.relax_bf_rate_controller();
attitude_control.set_yaw_target_to_current_heading();
attitude_control.set_throttle_out(0, false);
pos_control.set_alt_target_to_current_alt();
return;
}
// process pilot inputs
if (!failsafe.radio) {
// get pilot's desired yaw rate
target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in);
if (target_yaw_rate != 0) {
circle_pilot_yaw_override = true;
}
// get pilot desired climb rate
target_climb_rate = get_pilot_desired_climb_rate(g.rc_3.control_in);
// check for pilot requested take-off
if (ap.land_complete && target_climb_rate > 0) {
// indicate we are taking off
set_land_complete(false);
// clear i term when we're taking off
set_throttle_takeoff();
}
}
// run circle controller
circle_nav.update();
// call attitude controller
if (circle_pilot_yaw_override) {
attitude_control.angle_ef_roll_pitch_rate_ef_yaw(circle_nav.get_roll(), circle_nav.get_pitch(), target_yaw_rate);
}else{
attitude_control.angle_ef_roll_pitch_yaw(circle_nav.get_roll(), circle_nav.get_pitch(), circle_nav.get_yaw(),true);
}
// run altitude controller
if (sonar_alt_health >= SONAR_ALT_HEALTH_MAX) {
// if sonar is ok, use surface tracking
target_climb_rate = get_throttle_surface_tracking(target_climb_rate, pos_control.get_alt_target(), G_Dt);
}
// update altitude target and call position controller
pos_control.set_alt_target_from_climb_rate(target_climb_rate, G_Dt);
pos_control.update_z_controller();
}