Fixed-wing unmanned aerial vehicle rolling maneuvering control method
A control method and unmanned aerial vehicle technology, applied in the direction of attitude control, etc., can solve the problems of inability to switch between forward flight and inverted flight state, lack of fast maneuvering target simulation ability, and inability to realize rapid rollover maneuvering flight actions, etc.
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[0049] The present invention will be further elaborated and illustrated below in conjunction with the accompanying drawings and specific embodiments. The technical features of the various implementations in the present invention can be combined accordingly on the premise that there is no conflict with each other.
[0050] The invention is used on a fixed-wing unmanned aerial vehicle, and is used to control the fixed-wing unmanned aerial vehicle to realize the switching between the forward flying state and the inverted flying state and the rapid adjustment of the flight direction through rolling and pitching. The UAV needs to be equipped with a multi-antenna satellite navigation and positioning system to ensure that the satellite navigation system can work normally during the maneuvering flight and to ensure the convergence of the inertial navigation system error. as attached figure 1 As shown, more than three satellite navigation antennas are evenly arranged on the head of th...
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