首页 | 本学科首页   官方微博 | 高级检索  
     检索      

飞行逆动力学的应用
引用本文:张曙光.飞行逆动力学的应用[J].北京航空航天大学学报,1998,24(5):563-566.
作者姓名:张曙光
作者单位:1. 北京航空航天大学 飞行器设计与应用力学系;
2. 空军工程学院 基础部
基金项目:航空科学基金(96A51016)资助项目
摘    要:考察了求解输入类飞行逆动力学问题的微分-迭代与积分-迭代算法; 探讨了利用逆动力学确定过失速机动操纵效能要求问题,这构成了进一步提出过失速机动飞机设计简化判据的数值基础; 利用逆动力学设计机动发生模块进行飞控系统的最外环控制,以便跟踪期望的复杂机动轨迹.飞机最速反向示例及其它数值仿真结果表明设计思想与算法是可行的.

关 键 词:逆问题  操纵性  飞行控制  操纵效能要求  机动发生模块
收稿时间:1997-06-27
修稿时间:: 1997-06-27

Applications of Inverse Flight Dynamics
Zhang Shuguang,Fang Zhenping,Wang Yong.Applications of Inverse Flight Dynamics[J].Journal of Beijing University of Aeronautics and Astronautics,1998,24(5):563-566.
Authors:Zhang Shuguang  Fang Zhenping  Wang Yong
Institution:1. Beijing University of Aeronautics and Astronautics,Dept.of Flight Vehicle Design and Applied Mechanics;
2. Air Force College of Engineering, Section of Elementary Disciplines
Abstract:Two computational techniques for inverse fight dynamics, namely derivation iteration and integration iteration techniques, are investigated.The application of inverse dynamics to determine control power requirements for post stall maneuvering is researched, and a maneuvering flight trajectory based algorithm is provided, which lays a numerical foundation for simplifying design criteria for post stall aircraft.With the model of inverse dynamics employed, a flight control mode for the outermost loop of the control system, named maneuver generator, is designed to follow desired complicated maneuvering flight trajectories.An example of rapid heading reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea.
Keywords:inverse problem  controllability  flight control  control power requirements  maneuver generator
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号