#include "Plane.h" Mode *Plane::mode_from_mode_num(const enum Mode::Number num) { Mode *ret = nullptr; switch (num) { case Mode::Number::MANUAL: ret = &mode_manual; break; case Mode::Number::CIRCLE: ret = &mode_circle; break; case Mode::Number::STABILIZE: ret = &mode_stabilize; break; case Mode::Number::TRAINING: ret = &mode_training; break; case Mode::Number::ACRO: ret = &mode_acro; break; case Mode::Number::FLY_BY_WIRE_A: ret = &mode_fbwa; break; case Mode::Number::FLY_BY_WIRE_B: ret = &mode_fbwb; break; case Mode::Number::CRUISE: ret = &mode_cruise; break; case Mode::Number::AUTOTUNE: ret = &mode_autotune; break; case Mode::Number::AUTO: ret = &mode_auto; break; case Mode::Number::RTL: ret = &mode_rtl; break; case Mode::Number::LOITER: ret = &mode_loiter; break; case Mode::Number::AVOID_ADSB: #if HAL_ADSB_ENABLED ret = &mode_avoidADSB; break; #endif // if ADSB is not compiled in then fallthrough to guided case Mode::Number::GUIDED: ret = &mode_guided; break; case Mode::Number::INITIALISING: ret = &mode_initializing; break; case Mode::Number::QSTABILIZE: ret = &mode_qstabilize; break; case Mode::Number::QHOVER: ret = &mode_qhover; break; case Mode::Number::QLOITER: ret = &mode_qloiter; break; case Mode::Number::QLAND: ret = &mode_qland; break; case Mode::Number::QRTL: ret = &mode_qrtl; break; case Mode::Number::QACRO: ret = &mode_qacro; break; case Mode::Number::QAUTOTUNE: ret = &mode_qautotune; break; case Mode::Number::TAKEOFF: ret = &mode_takeoff; break; case Mode::Number::THERMAL: #if HAL_SOARING_ENABLED ret = &mode_thermal; #endif break; } return ret; } void Plane::read_control_switch() { static bool switch_debouncer; uint8_t switchPosition = readSwitch(); // If switchPosition = 255 this indicates that the mode control channel input was out of range // If we get this value we do not want to change modes. if(switchPosition == 255) return; if (failsafe.rc_failsafe || failsafe.throttle_counter > 0) { // when we are in rc_failsafe mode then RC input is not // working, and we need to ignore the mode switch channel return; } if (millis() - failsafe.last_valid_rc_ms > 100) { // only use signals that are less than 0.1s old. return; } if (oldSwitchPosition != switchPosition) { if (switch_debouncer == false) { // this ensures that mode switches only happen if the // switch changes for 2 reads. This prevents momentary // spikes in the mode control channel from causing a mode // switch switch_debouncer = true; return; } set_mode_by_number((enum Mode::Number)flight_modes[switchPosition].get(), ModeReason::RC_COMMAND); oldSwitchPosition = switchPosition; } switch_debouncer = false; } uint8_t Plane::readSwitch(void) const { uint16_t pulsewidth = RC_Channels::get_radio_in(g.flight_mode_channel - 1); if (pulsewidth <= 900 || pulsewidth >= 2200) return 255; // This is an error condition if (pulsewidth <= 1230) return 0; if (pulsewidth <= 1360) return 1; if (pulsewidth <= 1490) return 2; if (pulsewidth <= 1620) return 3; if (pulsewidth <= 1749) return 4; // Software Manual return 5; // Hardware Manual } void Plane::reset_control_switch() { oldSwitchPosition = 254; read_control_switch(); } /* called when entering autotune */ void Plane::autotune_start(void) { gcs().send_text(MAV_SEVERITY_INFO, "Started autotune"); rollController.autotune_start(); pitchController.autotune_start(); } /* called when exiting autotune */ void Plane::autotune_restore(void) { rollController.autotune_restore(); pitchController.autotune_restore(); gcs().send_text(MAV_SEVERITY_INFO, "Stopped autotune"); } /* enable/disable autotune for AUTO modes */ void Plane::autotune_enable(bool enable) { if (enable) { autotune_start(); } else { autotune_restore(); } } /* are we flying inverted? */ bool Plane::fly_inverted(void) { if (control_mode == &plane.mode_manual) { return false; } if (inverted_flight) { // controlled with aux switch return true; } if (control_mode == &mode_auto && auto_state.inverted_flight) { return true; } return false; }