mirror of https://github.com/ArduPilot/ardupilot
91 lines
3.2 KiB
C++
91 lines
3.2 KiB
C++
#include "mode.h"
|
|
#include "Plane.h"
|
|
|
|
bool ModeAuto::_enter()
|
|
{
|
|
plane.throttle_allows_nudging = true;
|
|
plane.auto_throttle_mode = true;
|
|
plane.auto_navigation_mode = true;
|
|
if (plane.quadplane.available() && plane.quadplane.enable == 2) {
|
|
plane.auto_state.vtol_mode = true;
|
|
} else {
|
|
plane.auto_state.vtol_mode = false;
|
|
}
|
|
plane.next_WP_loc = plane.prev_WP_loc = plane.current_loc;
|
|
// start or resume the mission, based on MIS_AUTORESET
|
|
plane.mission.start_or_resume();
|
|
|
|
if (hal.util->was_watchdog_armed()) {
|
|
if (hal.util->persistent_data.waypoint_num != 0) {
|
|
gcs().send_text(MAV_SEVERITY_INFO, "Watchdog: resume WP %u", hal.util->persistent_data.waypoint_num);
|
|
plane.mission.set_current_cmd(hal.util->persistent_data.waypoint_num);
|
|
hal.util->persistent_data.waypoint_num = 0;
|
|
}
|
|
}
|
|
|
|
#if SOARING_ENABLED == ENABLED
|
|
plane.g2.soaring_controller.init_cruising();
|
|
#endif
|
|
|
|
return true;
|
|
}
|
|
|
|
void ModeAuto::_exit()
|
|
{
|
|
if (plane.mission.state() == AP_Mission::MISSION_RUNNING) {
|
|
plane.mission.stop();
|
|
|
|
if (plane.mission.get_current_nav_cmd().id == MAV_CMD_NAV_LAND &&
|
|
!plane.quadplane.is_vtol_land(plane.mission.get_current_nav_cmd().id))
|
|
{
|
|
plane.landing.restart_landing_sequence();
|
|
}
|
|
}
|
|
plane.auto_state.started_flying_in_auto_ms = 0;
|
|
}
|
|
|
|
void ModeAuto::update()
|
|
{
|
|
if (plane.mission.state() != AP_Mission::MISSION_RUNNING) {
|
|
// this could happen if AP_Landing::restart_landing_sequence() returns false which would only happen if:
|
|
// restart_landing_sequence() is called when not executing a NAV_LAND or there is no previous nav point
|
|
plane.set_mode(plane.mode_rtl, MODE_REASON_MISSION_END);
|
|
gcs().send_text(MAV_SEVERITY_INFO, "Aircraft in auto without a running mission");
|
|
return;
|
|
}
|
|
|
|
uint16_t nav_cmd_id = plane.mission.get_current_nav_cmd().id;
|
|
|
|
if (plane.quadplane.in_vtol_auto()) {
|
|
plane.quadplane.control_auto(plane.next_WP_loc);
|
|
} else if (nav_cmd_id == MAV_CMD_NAV_TAKEOFF ||
|
|
(nav_cmd_id == MAV_CMD_NAV_LAND && plane.flight_stage == AP_Vehicle::FixedWing::FLIGHT_ABORT_LAND)) {
|
|
plane.takeoff_calc_roll();
|
|
plane.takeoff_calc_pitch();
|
|
plane.calc_throttle();
|
|
} else if (nav_cmd_id == MAV_CMD_NAV_LAND) {
|
|
plane.calc_nav_roll();
|
|
plane.calc_nav_pitch();
|
|
|
|
// allow landing to restrict the roll limits
|
|
plane.nav_roll_cd = plane.landing.constrain_roll(plane.nav_roll_cd, plane.g.level_roll_limit*100UL);
|
|
|
|
if (plane.landing.is_throttle_suppressed()) {
|
|
// if landing is considered complete throttle is never allowed, regardless of landing type
|
|
SRV_Channels::set_output_scaled(SRV_Channel::k_throttle, 0);
|
|
} else {
|
|
plane.calc_throttle();
|
|
}
|
|
} else {
|
|
// we are doing normal AUTO flight, the special cases
|
|
// are for takeoff and landing
|
|
if (nav_cmd_id != MAV_CMD_NAV_CONTINUE_AND_CHANGE_ALT) {
|
|
plane.steer_state.hold_course_cd = -1;
|
|
}
|
|
plane.calc_nav_roll();
|
|
plane.calc_nav_pitch();
|
|
plane.calc_throttle();
|
|
}
|
|
}
|
|
|