| 飞行轨迹指令综合跟踪控制器设计 |
| |
| 引用本文： | 邱晓红,高金源,张林昌.飞行轨迹指令综合跟踪控制器设计[J].航空学报,1997,18(4):407-411. |
| |
| 作者姓名： | 邱晓红 高金源 张林昌 |
| |
| 作者单位： | 北京航空航天大学无人机所 |
| |
| 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： | 奇异摄动理论 线性化 优化 非线性解耦控制 飞行管理系统 |
| 收稿时间： | 1996-07-19; |
DESIGN OF FLIGHT TRAJECTORY COMMAND INTEGRATED TRACKER |
| |
| Qiu Xiaohong,Gao Jinyuan,Zhang Linchang.DESIGN OF FLIGHT TRAJECTORY COMMAND INTEGRATED TRACKER[J].Acta Aeronautica et Astronautica Sinica,1997,18(4):407-411. |
| |
| Authors: | Qiu Xiaohong Gao Jinyuan Zhang Linchang |
| |
| Institution: | Research Institute of Unmanned Aerial Vehicle,Beijing University of Aeronautics and Astronautics, Beijing,100083 |
| |
| Abstract: | A systematic design method for flight trajectory command integrated 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 scales. |
| |
| Keywords: | singular perturbation theory linearization optimization nonlinear decoupling control flight management system |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航空学报》浏览原始摘要信息 |
| 点击此处可从《航空学报》下载免费的PDF全文 |
