2017-02-26 19:18:38 -04:00
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#include "Plane.h"
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2018-07-29 19:57:55 -03:00
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#if SOARING_ENABLED == ENABLED
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2017-02-26 19:18:38 -04:00
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/*
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* ArduSoar support function
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*
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* Peter Braswell, Samuel Tabor, Andrey Kolobov, and Iain Guilliard
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*/
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void Plane::update_soaring() {
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2019-07-15 07:27:29 -03:00
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// Check if soaring is active. Also sets throttle suppressed
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// status on active state changes.
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2020-04-05 08:38:19 -03:00
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plane.g2.soaring_controller.update_active_state();
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if (!g2.soaring_controller.is_active()) {
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2017-02-26 19:18:38 -04:00
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return;
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}
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g2.soaring_controller.update_vario();
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// Check for throttle suppression change.
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2019-01-15 13:46:13 -04:00
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switch (control_mode->mode_number()) {
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case Mode::Number::AUTO:
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2017-02-26 19:18:38 -04:00
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g2.soaring_controller.suppress_throttle();
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break;
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2019-01-15 13:46:13 -04:00
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case Mode::Number::FLY_BY_WIRE_B:
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case Mode::Number::CRUISE:
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2018-10-18 09:51:21 -03:00
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if (!g2.soaring_controller.suppress_throttle() && aparm.throttle_max > 0) {
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2017-07-09 00:49:39 -03:00
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gcs().send_text(MAV_SEVERITY_INFO, "Soaring: forcing RTL");
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2019-10-17 00:49:32 -03:00
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set_mode(mode_rtl, ModeReason::SOARING_FBW_B_WITH_MOTOR_RUNNING);
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2017-02-26 19:18:38 -04:00
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}
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break;
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2019-01-15 13:46:13 -04:00
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case Mode::Number::LOITER:
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2018-10-18 09:51:21 -03:00
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// Never use throttle in LOITER with soaring active.
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g2.soaring_controller.set_throttle_suppressed(true);
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2017-02-26 19:18:38 -04:00
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break;
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default:
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2018-10-18 09:51:21 -03:00
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// In any other mode allow throttle.
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g2.soaring_controller.set_throttle_suppressed(false);
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2017-02-26 19:18:38 -04:00
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break;
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}
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// Nothing to do if we are in powered flight
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if (!g2.soaring_controller.get_throttle_suppressed() && aparm.throttle_max > 0) {
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return;
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}
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2019-01-15 13:46:13 -04:00
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switch (control_mode->mode_number()) {
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2019-06-05 15:24:17 -03:00
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default:
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// nothing to do
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break;
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2019-01-15 13:46:13 -04:00
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case Mode::Number::AUTO:
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case Mode::Number::FLY_BY_WIRE_B:
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case Mode::Number::CRUISE:
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2017-02-26 19:18:38 -04:00
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// Test for switch into thermalling mode
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g2.soaring_controller.update_cruising();
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if (g2.soaring_controller.check_thermal_criteria()) {
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2019-06-05 15:24:17 -03:00
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gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Thermal detected, entering %s", mode_loiter.name());
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2019-10-17 00:49:32 -03:00
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set_mode(mode_loiter, ModeReason::SOARING_THERMAL_DETECTED);
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2017-02-26 19:18:38 -04:00
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}
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break;
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2019-06-05 15:24:17 -03:00
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case Mode::Number::LOITER: {
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2017-02-26 19:18:38 -04:00
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// Update thermal estimate and check for switch back to AUTO
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g2.soaring_controller.update_thermalling(); // Update estimate
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2020-06-26 14:04:19 -03:00
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// Thermalling is done in a home-relative coordinate system, so we need home to be set.
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Vector3f position;
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if (!ahrs.get_relative_position_NED_home(position)) {
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return;
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}
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// Check distance to home against MAX_RADIUS.
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if (g2.soaring_controller.max_radius >= 0 &&
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powf(position.x,2)+powf(position.y,2) > powf(g2.soaring_controller.max_radius,2) &&
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previous_mode->mode_number()!=Mode::Number::AUTO) {
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// Some other loiter status, and outside of maximum soaring radius, and previous mode wasn't AUTO
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gcs().send_text(MAV_SEVERITY_INFO, "Soaring: Outside SOAR_MAX_RADIUS, RTL");
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set_mode(mode_rtl, ModeReason::SOARING_DRIFT_EXCEEDED);
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break;
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}
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// If previous mode was AUTO and there was a previous NAV command, we can use previous and next wps for drift calculation
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// with respect to the desired direction of travel. If these vectors are zero, drift will be calculated from thermal start
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// position only, without taking account of the desired direction of travel.
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2019-06-22 14:51:17 -03:00
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Vector2f prev_wp, next_wp;
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2020-06-26 14:04:19 -03:00
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if (previous_mode == &mode_auto) {
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2019-06-22 14:51:17 -03:00
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AP_Mission::Mission_Command current_nav_cmd = mission.get_current_nav_cmd();
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AP_Mission::Mission_Command prev_nav_cmd;
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if (!(mission.get_next_nav_cmd(mission.get_prev_nav_cmd_with_wp_index(), prev_nav_cmd) &&
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2020-06-26 14:04:19 -03:00
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prev_nav_cmd.content.location.get_vector_xy_from_origin_NE(prev_wp) &&
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2019-06-22 14:51:17 -03:00
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current_nav_cmd.content.location.get_vector_xy_from_origin_NE(next_wp))) {
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2020-06-26 14:04:19 -03:00
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prev_wp.zero();
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next_wp.zero();
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2019-06-22 14:51:17 -03:00
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}
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}
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2020-06-26 14:04:19 -03:00
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// Get the status of the soaring controller cruise checks.
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2019-06-22 14:51:17 -03:00
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const SoaringController::LoiterStatus loiterStatus = g2.soaring_controller.check_cruise_criteria(prev_wp/100, next_wp/100);
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2017-02-26 19:18:38 -04:00
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2020-04-05 08:38:19 -03:00
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if (loiterStatus == SoaringController::LoiterStatus::GOOD_TO_KEEP_LOITERING) {
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2019-06-08 21:25:01 -03:00
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// Reset loiter angle, so that the loiter exit heading criteria
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// only starts expanding when we're ready to exit.
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plane.loiter.sum_cd = 0;
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2020-06-26 14:04:19 -03:00
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plane.soaring_mode_timer_ms = AP_HAL::millis();
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//update the wp location
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g2.soaring_controller.get_target(next_WP_loc);
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2019-06-05 15:24:17 -03:00
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break;
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}
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2017-02-26 19:18:38 -04:00
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2019-06-10 14:07:24 -03:00
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// Some other loiter status, we need to think about exiting loiter.
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2020-06-26 14:04:19 -03:00
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const uint32_t time_in_loiter_ms = AP_HAL::millis() - plane.soaring_mode_timer_ms;
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2019-06-10 14:07:24 -03:00
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2020-06-26 14:04:19 -03:00
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if (!soaring_exit_heading_aligned() && loiterStatus!=SoaringController::LoiterStatus::ALT_TOO_LOW && time_in_loiter_ms < 20000) {
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// Heading not lined up, and not timed out or in a condition requiring immediate exit.
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break;
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2019-06-17 09:15:53 -03:00
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}
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2020-06-26 14:04:19 -03:00
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// Heading lined up and loiter status not good to continue. Need to switch mode.
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2019-06-05 15:24:17 -03:00
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2020-06-26 14:04:19 -03:00
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// Determine appropriate mode.
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Mode* exit_mode = previous_mode;
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if (loiterStatus == SoaringController::LoiterStatus::ALT_TOO_LOW &&
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((previous_mode == &mode_cruise) || (previous_mode == &mode_fbwb))) {
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exit_mode = &mode_rtl;
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}
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// Print message and set mode.
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switch (loiterStatus) {
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case SoaringController::LoiterStatus::ALT_TOO_HIGH:
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soaring_restore_mode("Too high", ModeReason::SOARING_ALT_TOO_HIGH, *exit_mode);
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2019-06-05 15:24:17 -03:00
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break;
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2020-06-26 14:04:19 -03:00
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case SoaringController::LoiterStatus::ALT_TOO_LOW:
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soaring_restore_mode("Too low", ModeReason::SOARING_ALT_TOO_LOW, *exit_mode);
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break;
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default:
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case SoaringController::LoiterStatus::THERMAL_WEAK:
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soaring_restore_mode("Thermal ended", ModeReason::SOARING_THERMAL_ESTIMATE_DETERIORATED, *exit_mode);
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2019-06-05 15:24:17 -03:00
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break;
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2020-06-26 14:04:19 -03:00
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case SoaringController::LoiterStatus::DRIFT_EXCEEDED:
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soaring_restore_mode("Drifted too far", ModeReason::SOARING_DRIFT_EXCEEDED, *exit_mode);
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2019-06-05 15:24:17 -03:00
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break;
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2020-06-26 14:04:19 -03:00
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} // switch loiterStatus
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2017-02-26 19:18:38 -04:00
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break;
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2020-06-26 14:04:19 -03:00
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} // case loiter
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2019-06-05 17:04:20 -03:00
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} // switch control_mode
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2020-06-26 14:04:19 -03:00
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}
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2019-06-05 15:24:17 -03:00
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2020-06-26 14:04:19 -03:00
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bool Plane::soaring_exit_heading_aligned() const
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{
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// Return true if the current heading is aligned with the next objective.
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// If home is not set, or heading not locked, return true to avoid delaying mode change.
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switch (previous_mode->mode_number()) {
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case Mode::Number::AUTO: {
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//Get the lat/lon of next Nav waypoint after this one:
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AP_Mission::Mission_Command current_nav_cmd = mission.get_current_nav_cmd();;
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return plane.mode_loiter.isHeadingLinedUp(next_WP_loc, current_nav_cmd.content.location);
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2017-02-26 19:18:38 -04:00
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}
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2020-06-26 14:04:19 -03:00
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case Mode::Number::FLY_BY_WIRE_B:
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return (!AP::ahrs().home_is_set() || plane.mode_loiter.isHeadingLinedUp(next_WP_loc, AP::ahrs().get_home()));
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case Mode::Number::CRUISE:
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return (!cruise_state.locked_heading || plane.mode_loiter.isHeadingLinedUp_cd(cruise_state.locked_heading_cd));
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default:
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break;
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}
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return true;
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}
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2019-06-05 15:24:17 -03:00
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2020-06-26 14:04:19 -03:00
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void Plane::soaring_restore_mode(const char *reason, ModeReason modereason, Mode &exit_mode)
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{
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gcs().send_text(MAV_SEVERITY_INFO, "Soaring: %s, restoring %s", reason, exit_mode.name());
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set_mode(exit_mode, modereason);
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2017-02-26 19:18:38 -04:00
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}
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2018-07-29 19:57:55 -03:00
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#endif // SOARING_ENABLED
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