Control method of morphing aircraft, controller and application of morphing aircraft

The invention provides a control method of a morphing aircraft, and the method comprises the steps: obtaining the flight data of a left wing and a right wing, the flight data at least comprises a hinge rotation included angle between a first fixed wing and a first connecting rod, a hinge rotation in...

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Bibliographic Details
Main Authors CHEN HAIXIN, ZHU CHENHUA, FENG LIANGTAO, GUO TINGYU
Format Patent
LanguageChinese
English
Published 15.03.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention provides a control method of a morphing aircraft, and the method comprises the steps: obtaining the flight data of a left wing and a right wing, the flight data at least comprises a hinge rotation included angle between a first fixed wing and a first connecting rod, a hinge rotation included angle between a first movable wing and the first connecting rod, a hinge rotation included angle between a second fixed wing and a second connecting rod and a hinge rotation included angle between a second movable wing and the second connecting rod; inputting the flight data into a control model of the morphing aircraft for simulation calculation, and outputting a control quantity; according to the control quantity, the postures of the first movable wing and the second movable wing are adjusted, so that the first movable wing and the second movable wing move from the folding position to the unfolding position after the morphing aircraft ascends to the preset height, or the first movable wing and the second m
Bibliography:Application Number: CN202111608140