系统仿真学报 ›› 2015, Vol. 27 ›› Issue (7): 1435-1443.

• 建模与仿真理论及方法 • 上一篇    下一篇

机动飞行状态下飞行员人体动态体表力建模研究

刘刚, 王云普, 迟宏伟, 袁洪印   

  1. 长春科技学院汽车机械工程学院,吉林 长春 130600
  • 收稿日期:2014-06-17 修回日期:2014-09-24 出版日期:2015-07-08 发布日期:2020-07-31
  • 作者简介:刘刚(1961-),男,吉林长春人,博士,教授,研究方向为机械系统动力学及其仿真;王云普(1964-),男,吉林长春人,硕士,副教授,研究方向为动力机械及其仿真。
  • 基金资助:
    中国博士后科学基金(20080431390)

Modeling Research on Dynamic Pressure Distribution of Pilot Body in Maneuver Flight

Liu Gang, Wang Yunpu, Chi Hongwei, Yuan Hongyin   

  1. Department of Automobile and Mechanical Engineering, Changchun University of Science and Technology, Changchun 130600, China
  • Received:2014-06-17 Revised:2014-09-24 Online:2015-07-08 Published:2020-07-31

摘要: 对机动飞行时飞行员人体动态体表力分布与飞行过载之间的关系进行了研究。引入动态压力因子和剪力因子来表示坐姿飞行员人体动态体表压力和剪力分布建立了坐姿飞行员人体飞行动力学方程方程给出飞行员人体惯性力与体表力之间的关系,且关于动态压力因子和动态剪力因子二次非线性以某飞机上升转弯机动飞行为例,对飞行员人体动态体表力进行了数值仿真分析,数值结果符合飞行实际经验。此理论可用于飞行动态仿真过载椅的设计与控制。

关键词: 机动飞行, 动态体表力, 动力学方程, 过载椅

Abstract: Relationship between dynamic surface forces distribution of pilot body and flight load in maneuver flight was studied. Dynamic surface pressure and shear distribution of pilot body seated posture were expressed by setting up dynamic pressure factor and dynamic shear factor. Flight kinetic equations of pilot body seated posture were established. In the equations, relationship between pilot body inertia forces and dynamic surface forces were given, and the equations are square nonlinear for dynamic pressure factor and shear factor. Finally an example for climbing turn maneuver flight of some aircraft was done, dynamic surface forces distribution of pilot body were analyzed by numerical simulation, and the results meet the practical experience of pilot. The theory can be used to design and control the g-seat for flight dynamic simulation.

Key words: maneuver flight, dynamic surface force of body, kinetic equation, G-seat

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