mirror of https://github.com/ArduPilot/ardupilot
233 lines
8.0 KiB
C++
233 lines
8.0 KiB
C++
#include "Plane.h"
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Mode::Mode() :
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ahrs(plane.ahrs)
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#if HAL_QUADPLANE_ENABLED
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, quadplane(plane.quadplane),
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pos_control(plane.quadplane.pos_control),
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attitude_control(plane.quadplane.attitude_control),
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loiter_nav(plane.quadplane.loiter_nav),
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poscontrol(plane.quadplane.poscontrol)
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#endif
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{
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}
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void Mode::exit()
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{
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// call sub-classes exit
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_exit();
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// stop autotuning if not AUTOTUNE mode
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if (plane.control_mode != &plane.mode_autotune){
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plane.autotune_restore();
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}
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}
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bool Mode::enter()
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{
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#if AP_SCRIPTING_ENABLED
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// reset nav_scripting.enabled
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plane.nav_scripting.enabled = false;
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#endif
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// cancel inverted flight
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plane.auto_state.inverted_flight = false;
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// cancel waiting for rudder neutral
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plane.takeoff_state.waiting_for_rudder_neutral = false;
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// don't cross-track when starting a mission
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plane.auto_state.next_wp_crosstrack = false;
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// reset landing check
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plane.auto_state.checked_for_autoland = false;
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// zero locked course
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plane.steer_state.locked_course_err = 0;
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plane.steer_state.locked_course = false;
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// reset crash detection
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plane.crash_state.is_crashed = false;
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plane.crash_state.impact_detected = false;
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// reset external attitude guidance
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plane.guided_state.last_forced_rpy_ms.zero();
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plane.guided_state.last_forced_throttle_ms = 0;
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#if OFFBOARD_GUIDED == ENABLED
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plane.guided_state.target_heading = -4; // radians here are in range -3.14 to 3.14, so a default value needs to be outside that range
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plane.guided_state.target_heading_type = GUIDED_HEADING_NONE;
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plane.guided_state.target_airspeed_cm = -1; // same as above, although an airspeed of -1 is rare on plane.
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plane.guided_state.target_alt = -1; // same as above, although a target alt of -1 is rare on plane.
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plane.guided_state.last_target_alt = 0;
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#endif
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#if AP_CAMERA_ENABLED
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plane.camera.set_is_auto_mode(this == &plane.mode_auto);
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#endif
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// zero initial pitch and highest airspeed on mode change
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plane.auto_state.highest_airspeed = 0;
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plane.auto_state.initial_pitch_cd = ahrs.pitch_sensor;
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// disable taildrag takeoff on mode change
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plane.auto_state.fbwa_tdrag_takeoff_mode = false;
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// start with previous WP at current location
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plane.prev_WP_loc = plane.current_loc;
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// new mode means new loiter
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plane.loiter.start_time_ms = 0;
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// record time of mode change
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plane.last_mode_change_ms = AP_HAL::millis();
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// set VTOL auto state
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plane.auto_state.vtol_mode = is_vtol_mode();
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plane.auto_state.vtol_loiter = false;
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// initialize speed variable used in AUTO and GUIDED for DO_CHANGE_SPEED commands
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plane.new_airspeed_cm = -1;
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#if HAL_QUADPLANE_ENABLED
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quadplane.mode_enter();
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#endif
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bool enter_result = _enter();
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if (enter_result) {
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// -------------------
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// these must be done AFTER _enter() because they use the results to set more flags
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// start with throttle suppressed in auto_throttle modes
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plane.throttle_suppressed = does_auto_throttle();
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#if HAL_ADSB_ENABLED
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plane.adsb.set_is_auto_mode(does_auto_navigation());
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#endif
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// reset steering integrator on mode change
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plane.steerController.reset_I();
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// update RC failsafe, as mode change may have necessitated changing the failsafe throttle
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plane.control_failsafe();
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#if AP_FENCE_ENABLED
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// pilot requested flight mode change during a fence breach indicates pilot is attempting to manually recover
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// this flight mode change could be automatic (i.e. fence, battery, GPS or GCS failsafe)
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// but it should be harmless to disable the fence temporarily in these situations as well
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plane.fence.manual_recovery_start();
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#endif
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}
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return enter_result;
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}
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bool Mode::is_vtol_man_throttle() const
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{
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#if HAL_QUADPLANE_ENABLED
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if (plane.quadplane.tailsitter.is_in_fw_flight() &&
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plane.quadplane.assisted_flight) {
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// We are a tailsitter that has fully transitioned to Q-assisted forward flight.
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// In this case the forward throttle directly drives the vertical throttle so
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// set vertical throttle state to match the forward throttle state. Confusingly the booleans are inverted,
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// forward throttle uses 'does_auto_throttle' whereas vertical uses 'is_vtol_man_throttle'.
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return !does_auto_throttle();
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}
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#endif
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return false;
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}
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void Mode::update_target_altitude()
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{
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Location target_location;
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if (plane.landing.is_flaring()) {
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// during a landing flare, use TECS_LAND_SINK as a target sink
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// rate, and ignores the target altitude
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plane.set_target_altitude_location(plane.next_WP_loc);
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} else if (plane.landing.is_on_approach()) {
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plane.landing.setup_landing_glide_slope(plane.prev_WP_loc, plane.next_WP_loc, plane.current_loc, plane.target_altitude.offset_cm);
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plane.landing.adjust_landing_slope_for_rangefinder_bump(plane.rangefinder_state, plane.prev_WP_loc, plane.next_WP_loc, plane.current_loc, plane.auto_state.wp_distance, plane.target_altitude.offset_cm);
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} else if (plane.landing.get_target_altitude_location(target_location)) {
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plane.set_target_altitude_location(target_location);
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#if HAL_SOARING_ENABLED
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} else if (plane.g2.soaring_controller.is_active() && plane.g2.soaring_controller.get_throttle_suppressed()) {
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// Reset target alt to current alt, to prevent large altitude errors when gliding.
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plane.set_target_altitude_location(plane.current_loc);
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plane.reset_offset_altitude();
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#endif
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} else if (plane.reached_loiter_target()) {
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// once we reach a loiter target then lock to the final
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// altitude target
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plane.set_target_altitude_location(plane.next_WP_loc);
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} else if (plane.target_altitude.offset_cm != 0 &&
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!plane.current_loc.past_interval_finish_line(plane.prev_WP_loc, plane.next_WP_loc)) {
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// control climb/descent rate
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plane.set_target_altitude_proportion(plane.next_WP_loc, 1.0f-plane.auto_state.wp_proportion);
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// stay within the range of the start and end locations in altitude
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plane.constrain_target_altitude_location(plane.next_WP_loc, plane.prev_WP_loc);
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} else {
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plane.set_target_altitude_location(plane.next_WP_loc);
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}
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plane.altitude_error_cm = plane.calc_altitude_error_cm();
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}
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// returns true if the vehicle can be armed in this mode
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bool Mode::pre_arm_checks(size_t buflen, char *buffer) const
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{
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if (!_pre_arm_checks(buflen, buffer)) {
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if (strlen(buffer) == 0) {
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// If no message is provided add a generic one
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hal.util->snprintf(buffer, buflen, "mode not armable");
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}
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return false;
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}
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return true;
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}
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// Auto and Guided do not call this to bypass the q-mode check.
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bool Mode::_pre_arm_checks(size_t buflen, char *buffer) const
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{
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#if HAL_QUADPLANE_ENABLED
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if (plane.quadplane.enabled() && !is_vtol_mode() &&
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plane.quadplane.option_is_set(QuadPlane::OPTION::ONLY_ARM_IN_QMODE_OR_AUTO)) {
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hal.util->snprintf(buffer, buflen, "not Q mode");
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return false;
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}
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#endif
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return true;
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}
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void Mode::run()
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{
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// Direct stick mixing functionality has been removed, so as not to remove all stick mixing from the user completely
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// the old direct option is now used to enable fbw mixing, this is easier than doing a param conversion.
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if ((plane.g.stick_mixing == StickMixing::FBW) || (plane.g.stick_mixing == StickMixing::DIRECT_REMOVED)) {
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plane.stabilize_stick_mixing_fbw();
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}
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plane.stabilize_roll();
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plane.stabilize_pitch();
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plane.stabilize_yaw();
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}
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// Reset rate and steering controllers
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void Mode::reset_controllers()
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{
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// reset integrators
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plane.rollController.reset_I();
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plane.pitchController.reset_I();
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plane.yawController.reset_I();
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// reset steering controls
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plane.steer_state.locked_course = false;
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plane.steer_state.locked_course_err = 0;
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}
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bool Mode::is_taking_off() const
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{
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return (plane.flight_stage == AP_FixedWing::FlightStage::TAKEOFF);
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}
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