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https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-25 08:36:08 +08:00
add minimal pitch field to mission item
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@@ -103,11 +103,20 @@ int map_mavlink_mission_item_to_mission_item(const mavlink_mission_item_t *mavli
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return MAV_MISSION_ERROR;
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}
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switch (mavlink_mission_item->command) {
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case MAV_CMD_NAV_TAKEOFF:
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mission_item->pitch_min = mavlink_mission_item->param1;
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break;
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default:
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mission_item->radius = mavlink_mission_item->param1;
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break;
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}
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mission_item->yaw = _wrap_pi(mavlink_mission_item->param4*M_DEG_TO_RAD_F);
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mission_item->loiter_radius = fabsf(mavlink_mission_item->param3);
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mission_item->loiter_direction = (mavlink_mission_item->param3 > 0) ? 1 : -1; /* 1 if positive CW, -1 if negative CCW */
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mission_item->nav_cmd = mavlink_mission_item->command;
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mission_item->radius = mavlink_mission_item->param1;
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mission_item->time_inside = mavlink_mission_item->param2 / 1e3f; /* from milliseconds to seconds */
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mission_item->autocontinue = mavlink_mission_item->autocontinue;
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mission_item->index = mavlink_mission_item->seq;
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@@ -89,6 +89,7 @@ struct mission_item_s
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enum NAV_CMD nav_cmd; /**< navigation command */
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float radius; /**< radius in which the mission is accepted as reached in meters */
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float time_inside; /**< time that the MAV should stay inside the radius before advancing in seconds */
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float pitch_min; /**< minimal pitch angle for fixed wing takeoff waypoints */
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bool autocontinue; /**< true if next waypoint should follow after this one */
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int index; /**< index matching the mavlink waypoint */
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enum ORIGIN origin; /**< where the waypoint has been generated */
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