Flexible aircraft control method based on wing structure transformation

The invention relates to the field of aircraft control, in particular to a flexible aircraft control method based on wing structure transformation. According to the method, wings of an aircraft are telescopic wings and the height is flexible, wherein the wings on the two sides symmetrically stretch...

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Bibliographic Details
Main Authors GUO ZHENG, LIU DUONENG, LIU ZHAOWEI, GUO TIANHAO, JIANG JIE, HOU ZHONGXI, MA ZHENYU, YANG XIXIANG
Format Patent
LanguageChinese
English
Published 16.03.2016
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention relates to the field of aircraft control, in particular to a flexible aircraft control method based on wing structure transformation. According to the method, wings of an aircraft are telescopic wings and the height is flexible, wherein the wings on the two sides symmetrically stretch or retract to increase or reduce the lifting force of the aircraft and the lifting weight balance of the aircraft is changed; and the navigation direction is flexible, wherein the wings on the two sides asymmetrically stretch or retract, the lifting force difference is generated by the wings on the two sides of the aircraft, the rolling moment is generated, and the aircraft inclines. By the adoption of the method, the lifting force is increased or reduced to directly achieve height flexibility, and changes of the angle of pitch generated when the height is changed are greatly reduced; the wings on the two sides asymmetrically stretch or retract to achieve navigation direction flexibility, compared with an existing
Bibliography:Application Number: CN20151809073