forked from Archive/PX4-Autopilot
rtl_direct_mission: rtl_estimate for fixedwing land is diagonal
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89844625b4
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@ -308,8 +308,6 @@ rtl_time_estimate_s RtlDirectMissionLand::calc_rtl_time_estimate()
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break;
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}
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case NAV_CMD_LAND: // Fallthrough
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case NAV_CMD_VTOL_LAND: // Fallthrough
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case NAV_CMD_LOITER_TO_ALT: {
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// Go to point horizontally
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matrix::Vector2f direction{};
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@ -327,6 +325,34 @@ rtl_time_estimate_s RtlDirectMissionLand::calc_rtl_time_estimate()
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break;
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}
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case NAV_CMD_LAND: // Fallthrough
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case NAV_CMD_VTOL_LAND: {
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matrix::Vector2f direction{};
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get_vector_to_next_waypoint(hor_position_at_calculation_point(0), hor_position_at_calculation_point(1),
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next_position_mission_item.lat, next_position_mission_item.lon, &direction(0), &direction(1));
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float hor_dist = get_distance_to_next_waypoint(hor_position_at_calculation_point(0),
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hor_position_at_calculation_point(1), next_position_mission_item.lat, next_position_mission_item.lon);
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// For fixed wing, add diagonal line
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if ((_vehicle_status_sub.get().vehicle_type != vehicle_status_s::VEHICLE_TYPE_FIXED_WING)
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&& (!_vehicle_status_sub.get().is_vtol)) {
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_rtl_time_estimator.addDistance(hor_dist, direction,
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next_position_mission_item.altitude - altitude_at_calculation_point);
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} else {
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// For VTOL, Rotary, go there horizontally first, then land
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_rtl_time_estimator.addDistance(hor_dist, direction, 0.f);
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_rtl_time_estimator.addDescendMCLand(next_position_mission_item.altitude - altitude_at_calculation_point);
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}
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break;
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}
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default: {
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// Default assume can go to the location directly
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matrix::Vector2f direction{};
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