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综合飞行轨迹指令跟踪控制器设计
引用本文:邱晓红,高金源.综合飞行轨迹指令跟踪控制器设计[J].北京航空航天大学学报,1997,23(6):745-750.
作者姓名:邱晓红  高金源
作者单位:北京航空航天大学自动控制系
摘    要:运用多重尺度奇异摄动理论,结合动态逆解耦理论和动态平衡点邻区域优化线性化系统的优化解耦控制律理论,研究了战术任务综合飞行管理系统的综合飞行轨迹指令跟踪控制器系统化设计方法。对F-15飞机,设计了综合飞行轨迹跟踪控制器。数字仿真结果表明,设计的跟踪控制器能够控制飞机精确跟踪不同时标集的飞行指令。

关 键 词:飞行轨迹  跟踪控制器  飞行管理系统

DESIGN OF INTEGRATED FLIGHT TRAJECTORY COMMAND TRACKER
Qiu Xiaohong,Gao Jinyuan,Zhang Linchang.DESIGN OF INTEGRATED FLIGHT TRAJECTORY COMMAND TRACKER[J].Journal of Beijing University of Aeronautics and Astronautics,1997,23(6):745-750.
Authors:Qiu Xiaohong  Gao Jinyuan  Zhang Linchang
Abstract:A systematic design method for integrated flight trajectory command tracker of Tactical Mission Integrated Flight Management System(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method.The results of digital simulation show that the controller can control fighter track commands in different time scale.
Keywords:perturbation theory  linearization  optimization  non linear  decoupling  flight management systems
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