Autonomous fixed-point recovery method for parachute fixed-wing UAV
A technology of autonomous and recovery methods for fixed-wing UAVs, which is applied in the direction of three-dimensional position/channel control, etc., can solve the problems of inability to truly achieve autonomous recovery and manual upload of recovery routes, so as to reduce operational burden and simplify aircraft recovery The effect of operating procedures
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[0045] The present invention will be further described below in conjunction with the accompanying drawings and embodiments, and the present invention includes but not limited to the following embodiments.
[0046] The steps of the method involved in the present invention are as follows:
[0047] 1. Manually set the recovery point P(x 0 ,y 0 ) (in the north-east coordinate system) and recovery heading α.
[0048] 2. Determine whether the recycling setting meets the recycling conditions. The specific judgment steps are as follows:
[0049] 1) Generate a recycling area based on a given recycling point and recycling direction. The recycling area is a rectangle with length L and width W. where L=0.5(V smin +V smax ) T 0 , W=2(t s + h s / v d )V 0 , where V smin , V smax is the upper and lower bounds of safe parachute opening speed, the unit is m / s, t s is the time interval between aircraft parking and parachute opening, h s Safe height for the aircraft to open the para...
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