The invention belongs to the technical field of aviation aircraft flight control, and particularly relates to a spin wing ring type active stability augmentation air refueling taper sleeve drift suppression device and method. Compared with a traditional wing rudder type active stability augmentation taper sleeve, the wing face of the self-rotating wing ring type active stability augmentation taper sleeve is not directly connected with a driving steering engine, the overall structure is more compact, the structural strength is higher, and the safety risk in the releasing and recycling process is smaller. According to the method, the hose-taper sleeve combination swinging motion model established on the basis of the Lagrange equation can quantitatively reflect the influence of wing ring rotation on the swinging motion of the taper sleeve. According to the taper sleeve drift suppression scheme based on momentum ring control, the drift amplitude of the taper sleeve can be effectively suppressed, and the high-frequency dynamic response of the taper sleeve is weakened.

    本发明属于航空飞行器飞行控制技术领域,特别涉及自旋翼环式主动增稳空中加油锥套飘摆抑制装置及方法。本发明得到的自旋式主动增稳锥套,相对于传统翼舵式主动增稳锥套,自旋翼环式主动增稳锥套翼面不与驱动舵机直接连接,整体结构更加紧凑,结构强度更高,释放回收过程安全风险更小。本发明基于拉格朗日方程建立的软管‑锥套组合体飘摆运动模型,能够定量反映翼环旋转对于锥套飘摆运动的影响。本发明基于动量环控制的锥套飘摆抑制方案,能够有效抑制锥套的飘摆幅度,削弱锥套高频动态响应。


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    Title :

    Device and method for suppressing swinging of self-rotating wing ring type active stability augmentation air refueling taper sleeve


    Additional title:

    自旋翼环式主动增稳空中加油锥套飘摆抑制装置及方法


    Contributors:
    ZHU ZHE (author) / HUANG JIANGTAO (author) / SHAN ENGUANG (author) / DU XIN (author) / ZHANG SHENG (author) / WANG CHUNYANG (author) / WANG YINZHU (author) / HU FANGFANG (author) / CHEN XIAN (author) / TANG JIGANG (author)

    Publication date :

    2024-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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