ardupilot/ArduPlane/soaring.cpp

100 lines
3.2 KiB
C++
Raw Normal View History

#include "Plane.h"
#if SOARING_ENABLED == ENABLED
/*
* ArduSoar support function
*
* Peter Braswell, Samuel Tabor, Andrey Kolobov, and Iain Guilliard
*/
void Plane::update_soaring() {
if (!g2.soaring_controller.is_active()) {
return;
}
g2.soaring_controller.update_vario();
// Check for throttle suppression change.
switch (control_mode){
case AUTO:
g2.soaring_controller.suppress_throttle();
break;
case FLY_BY_WIRE_B:
case CRUISE:
if (!g2.soaring_controller.suppress_throttle()) {
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: forcing RTL");
set_mode(RTL, MODE_REASON_SOARING_FBW_B_WITH_MOTOR_RUNNING);
}
break;
case LOITER:
// Do nothing. We will switch back to auto/rtl before enabling throttle.
break;
default:
// This does not affect the throttle since suppressed is only checked in the above three modes.
// It ensures that the soaring always starts with throttle suppressed though.
g2.soaring_controller.set_throttle_suppressed(true);
break;
}
// Nothing to do if we are in powered flight
if (!g2.soaring_controller.get_throttle_suppressed() && aparm.throttle_max > 0) {
return;
}
switch (control_mode){
case AUTO:
case FLY_BY_WIRE_B:
case CRUISE:
// Test for switch into thermalling mode
g2.soaring_controller.update_cruising();
if (g2.soaring_controller.check_thermal_criteria()) {
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal detected, entering loiter");
set_mode(LOITER, MODE_REASON_SOARING_THERMAL_DETECTED);
}
break;
case LOITER:
// Update thermal estimate and check for switch back to AUTO
g2.soaring_controller.update_thermalling(); // Update estimate
if (g2.soaring_controller.check_cruise_criteria()) {
// Exit as soon as thermal state estimate deteriorates
switch (previous_mode) {
case FLY_BY_WIRE_B:
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, entering RTL");
set_mode(RTL, MODE_REASON_SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
case CRUISE: {
// return to cruise with old ground course
CruiseState cruise = cruise_state;
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, restoring CRUISE");
set_mode(CRUISE, MODE_REASON_SOARING_THERMAL_ESTIMATE_DETERIORATED);
cruise_state = cruise;
set_target_altitude_current();
break;
}
case AUTO:
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, restoring AUTO");
set_mode(AUTO, MODE_REASON_SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
default:
break;
}
} else {
// still in thermal - need to update the wp location
g2.soaring_controller.get_target(next_WP_loc);
}
break;
default:
// nothing to do
break;
}
}
#endif // SOARING_ENABLED