#include "Plane.h" #include "quadplane.h" #include "qautotune.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; #if HAL_QUADPLANE_ENABLED 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; #if QAUTOTUNE_ENABLED case Mode::Number::QAUTOTUNE: ret = &mode_qautotune; break; #endif #endif // HAL_QUADPLANE_ENABLED case Mode::Number::TAKEOFF: ret = &mode_takeoff; break; case Mode::Number::THERMAL: #if HAL_SOARING_ENABLED ret = &mode_thermal; #endif break; #if HAL_QUADPLANE_ENABLED case Mode::Number::LOITER_ALT_QLAND: ret = &mode_loiter_qland; break; #endif // HAL_QUADPLANE_ENABLED } return ret; } void RC_Channels_Plane::read_mode_switch() { if (millis() - plane.failsafe.last_valid_rc_ms > 100) { // only use signals that are less than 0.1s old. return; } RC_Channels::read_mode_switch(); } void RC_Channel_Plane::mode_switch_changed(modeswitch_pos_t new_pos) { if (new_pos < 0 || (uint8_t)new_pos > plane.num_flight_modes) { // should not have been called return; } plane.set_mode_by_number((Mode::Number)plane.flight_modes[new_pos].get(), ModeReason::RC_COMMAND); } /* called when entering autotune */ void Plane::autotune_start(void) { const bool tune_roll = g2.axis_bitmask.get() & int8_t(AutoTuneAxis::ROLL); const bool tune_pitch = g2.axis_bitmask.get() & int8_t(AutoTuneAxis::PITCH); const bool tune_yaw = g2.axis_bitmask.get() & int8_t(AutoTuneAxis::YAW); if (tune_roll || tune_pitch || tune_yaw) { gcs().send_text(MAV_SEVERITY_INFO, "Started autotune"); if (tune_roll) { rollController.autotune_start(); } if (tune_pitch) { pitchController.autotune_start(); } if (tune_yaw) { yawController.autotune_start(); } autotuning = true; gcs().send_text(MAV_SEVERITY_INFO, "Autotuning %s%s%s", tune_roll?"roll ":"", tune_pitch?"pitch ":"", tune_yaw?"yaw":""); } else { gcs().send_text(MAV_SEVERITY_INFO, "No axis selected for tuning!"); } } /* called when exiting autotune */ void Plane::autotune_restore(void) { rollController.autotune_restore(); pitchController.autotune_restore(); yawController.autotune_restore(); if (autotuning) { autotuning = false; 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; }