#include "Plane.h" Mode::Mode() { } void Mode::exit() { // call sub-classes exit _exit(); } bool Mode::enter() { // cancel inverted flight plane.auto_state.inverted_flight = false; // don't cross-track when starting a mission plane.auto_state.next_wp_crosstrack = false; // reset landing check plane.auto_state.checked_for_autoland = false; // zero locked course plane.steer_state.locked_course_err = 0; // reset crash detection plane.crash_state.is_crashed = false; plane.crash_state.impact_detected = false; // reset external attitude guidance plane.guided_state.last_forced_rpy_ms.zero(); plane.guided_state.last_forced_throttle_ms = 0; #if CAMERA == ENABLED plane.camera.set_is_auto_mode(this == &plane.mode_auto); #endif // zero initial pitch and highest airspeed on mode change plane.auto_state.highest_airspeed = 0; plane.auto_state.initial_pitch_cd = plane.ahrs.pitch_sensor; // disable taildrag takeoff on mode change plane.auto_state.fbwa_tdrag_takeoff_mode = false; // start with previous WP at current location plane.prev_WP_loc = plane.current_loc; // new mode means new loiter plane.loiter.start_time_ms = 0; // record time of mode change plane.last_mode_change_ms = AP_HAL::millis(); // assume non-VTOL mode plane.auto_state.vtol_mode = false; plane.auto_state.vtol_loiter = false; bool enter_result = _enter(); if (enter_result) { // ------------------- // these must be done AFTER _enter() because they use the results to set more flags // start with throttle suppressed in auto_throttle modes plane.throttle_suppressed = plane.auto_throttle_mode; plane.adsb.set_is_auto_mode(plane.auto_navigation_mode); // reset steering integrator on mode change plane.steerController.reset_I(); // update RC failsafe, as mode change may have necessitated changing the failsafe throttle plane.control_failsafe(); } return enter_result; }