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现代高性能飞机可收放起落架主要参数的确定
引用本文:杨国柱. 现代高性能飞机可收放起落架主要参数的确定[J]. 航空学报, 1987, 8(10): 459-466
作者姓名:杨国柱
作者单位:北京航空学院
摘    要:本文建议一种简便的方法确定起落架转轴的方向、放下位置和收入位置时起落架的回转角。文中应用矢量阐明在空间结构中刚体元件之间的相互关系,并主要采用坐标转换方法求得回转矩阵。便于计算机计算分析。

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收稿时间:1986-05-23;

DETERMINATION OF MAIN PAMETERS OF A RETRACTABLE LANDING GEAR FOR MODERN HIGH PERFORMANCE AiRCRAFTS
Yang Guozhu. DETERMINATION OF MAIN PAMETERS OF A RETRACTABLE LANDING GEAR FOR MODERN HIGH PERFORMANCE AiRCRAFTS[J]. Acta Aeronautica et Astronautica Sinica, 1987, 8(10): 459-466
Authors:Yang Guozhu
Affiliation:Beijing Institute of Aeronautics and Astronautics
Abstract:A simple and convenient method is presented in this paper to determine the pivoting direction, the angle o'f rotation of the landing gear from its down toup position, and the angle of rotation of the wheel axis. In addition, the vectoranalysis is applied to elucidate the relationship between the individual rigidbody components' of spatial configurations, and the rotation matrix is obtained mainly by the use of coordinate transformation The method described is suitable for computer computation.
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