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Plane: add reason to exit Thermal loiter and adjust LOW alt reaon to cause RTL

zr-v5.1
Tom Pittenger 6 years ago committed by Andrew Tridgell
parent
commit
f6396d7a6d
  1. 114
      ArduPlane/soaring.cpp
  2. 2
      libraries/AP_Vehicle/ModeReason.h

114
ArduPlane/soaring.cpp

@ -43,6 +43,9 @@ void Plane::update_soaring() {
} }
switch (control_mode->mode_number()) { switch (control_mode->mode_number()) {
default:
// nothing to do
break;
case Mode::Number::AUTO: case Mode::Number::AUTO:
case Mode::Number::FLY_BY_WIRE_B: case Mode::Number::FLY_BY_WIRE_B:
case Mode::Number::CRUISE: case Mode::Number::CRUISE:
@ -50,50 +53,101 @@ void Plane::update_soaring() {
g2.soaring_controller.update_cruising(); g2.soaring_controller.update_cruising();
if (g2.soaring_controller.check_thermal_criteria()) { if (g2.soaring_controller.check_thermal_criteria()) {
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal detected, entering loiter"); gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal detected, entering %s", mode_loiter.name());
set_mode(mode_loiter, ModeReason::SOARING_THERMAL_DETECTED); set_mode(mode_loiter, ModeReason::SOARING_THERMAL_DETECTED);
} }
break; break;
case Mode::Number::LOITER: case Mode::Number::LOITER: {
// Update thermal estimate and check for switch back to AUTO // Update thermal estimate and check for switch back to AUTO
g2.soaring_controller.update_thermalling(); // Update estimate g2.soaring_controller.update_thermalling(); // Update estimate
if (g2.soaring_controller.check_cruise_criteria()) { const SoaringController::LoiterStatus loiterStatus = g2.soaring_controller.check_cruise_criteria();
// Exit as soon as thermal state estimate deteriorates
switch (previous_mode->mode_number()) {
case Mode::Number::FLY_BY_WIRE_B:
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, entering RTL");
set_mode(mode_rtl, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
case Mode::Number::CRUISE: { if (loiterStatus == SoaringController::LoiterStatus::THERMAL_GOOD_TO_KEEP_LOITERING ||
// return to cruise with old ground course loiterStatus == SoaringController::LoiterStatus::SOARING_DISABLED) {
CruiseState cruise = cruise_state; break;
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, restoring CRUISE"); }
set_mode(mode_cruise, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED);
cruise_state = cruise;
set_target_altitude_current();
break;
}
case Mode::Number::AUTO: const char* strTooHigh = "Soaring: Too high, restoring ";
gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal ended, restoring AUTO"); const char* strTooLow = "Soaring: Too high, restoring ";
set_mode(mode_auto, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED); const char* strTooWeak = "Soaring: Thermal ended, restoring ";
break;
default: // Exit as soon as thermal state estimate deteriorates
switch (previous_mode->mode_number()) {
case Mode::Number::FLY_BY_WIRE_B: {
switch (loiterStatus) {
case SoaringController::LoiterStatus::ALT_TOO_HIGH:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooHigh, mode_fbwb.name());
set_mode(mode_fbwb, ModeReason::SOARING_ALT_TOO_HIGH);
break;
default:
case SoaringController::LoiterStatus::ALT_TOO_LOW:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooLow, mode_rtl.name());
set_mode(mode_rtl, ModeReason::SOARING_ALT_TOO_LOW);
break;
case SoaringController::LoiterStatus::THERMAL_WEAK:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooWeak, mode_fbwb.name());
set_mode(mode_fbwb, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
} // switch louterStatus
break; break;
case Mode::Number::CRUISE: {
// return to cruise with old ground course
const CruiseState cruise = cruise_state;
switch (loiterStatus) {
case SoaringController::LoiterStatus::ALT_TOO_HIGH:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooHigh, mode_cruise.name());
set_mode(mode_cruise, ModeReason::SOARING_ALT_TOO_HIGH);
break;
default:
case SoaringController::LoiterStatus::ALT_TOO_LOW:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooLow, mode_rtl.name());
set_mode(mode_rtl, ModeReason::SOARING_ALT_TOO_LOW);
break;
case SoaringController::LoiterStatus::THERMAL_WEAK:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooWeak, mode_cruise.name());
set_mode(mode_cruise, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
} // switch loiterStatus
cruise_state = cruise;
set_target_altitude_current();
break;
} }
} else {
// still in thermal - need to update the wp location case Mode::Number::AUTO:
g2.soaring_controller.get_target(next_WP_loc); switch (loiterStatus) {
} case SoaringController::LoiterStatus::ALT_TOO_HIGH:
break; gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooHigh, mode_auto.name());
default: set_mode(mode_auto, ModeReason::SOARING_ALT_TOO_HIGH);
// nothing to do break;
default:
case SoaringController::LoiterStatus::ALT_TOO_LOW:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooLow, mode_auto.name());
set_mode(mode_auto, ModeReason::SOARING_ALT_TOO_LOW);
break;
case SoaringController::LoiterStatus::THERMAL_WEAK:
gcs().send_text(MAV_SEVERITY_INFO, "%s%s", strTooWeak, mode_auto.name());
set_mode(mode_auto, ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED);
break;
} // switch loiterStatus
break;
default:
break;
} // switch previous_mode
break; break;
} // loiter case
}} // switch control_mode
if (control_mode == &mode_loiter) {
// still in thermal - need to update the wp location
g2.soaring_controller.get_target(next_WP_loc);
} }
} }
#endif // SOARING_ENABLED #endif // SOARING_ENABLED

2
libraries/AP_Vehicle/ModeReason.h

@ -53,4 +53,6 @@ enum class ModeReason : uint8_t {
UNAVAILABLE, UNAVAILABLE,
AUTOROTATION_START, AUTOROTATION_START,
AUTOROTATION_BAILOUT, AUTOROTATION_BAILOUT,
SOARING_ALT_TOO_HIGH,
SOARING_ALT_TOO_LOW,
}; };

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