Unmanned plane automatic flight control method capable of adjusting spiral wing posture
A technology of automatic flight control and wing attitude, applied in the direction of non-electric variable control, control/adjustment system, three-dimensional position/course control, etc., can solve the problems of unacceptable cost and failure rate, high assumption cost of control center, and low efficiency , to achieve the effect of solving fixed-point automatic flight, high-efficiency and low-cost operation
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[0018] The technical solution of the present invention is further described below, but the scope of protection is not limited to the description.
[0019] The invention provides a method for controlling the automatic flight of an unmanned aerial vehicle with an adjustable helix attitude, comprising the following steps:
[0020] ①Initialization: Initialize and self-inspect the system, judge the operation of each component in the system, and perform four actions of take-off, forward, backward, and descent, and adjust the balance attitude reference control amount during the action;
[0021] ② Way point detection: The user inputs the way point, the system records the way point input by the user and stores it as a way point set, connects every two adjacent way points in the way point set, and loops to sort the top two paths point as the current starting point and end point, proceed to step ③ and step ④ until there is only one path point left, then proceed to step ⑥;
[0022] ③Rout...
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