| 机动飞行指令跟踪系统的鲁棒动态逆设计 |
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| 引用本文： | 沈景来,高金源.机动飞行指令跟踪系统的鲁棒动态逆设计[J].航空学报,1998,19(5):592-596. |
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| 作者姓名： | 沈景来 高金源 |
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| 作者单位： | 北京航空航天大学305教研室,北京,100083 |
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| 摘 要： | 简要介绍了用非线性动态逆解耦方法设计面向机动飞行的指令跟踪系统的过程。为了提高动态逆的鲁棒性，详细介绍了利用μ－分析/综合方法设计鲁棒控制器的方法、步骤、经验和设计结果。仿真表明，所设计的鲁棒动态逆控制器是有效的。
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| 关 键 词： | 非线性解耦控制 鲁棒控制 机动飞行 |
ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS |
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| Shen Jinglai,Gao Jinyuan.ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS[J].Acta Aeronautica et Astronautica Sinica,1998,19(5):592-596. |
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| Authors: | Shen Jinglai Gao Jinyuan |
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| Institution: | Faculty 305, Beijing University of Aeronautics &; Astronautics, Beijing, 100083 |
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| Abstract: | The design of a maneuverable flight command tracking system using nonlinear dynamic inversion is briefly introduced at first. And then a robust controller to improve the robustness of dynamic inversion is designed using the method of μ analysis and synthesis. The detailed design process and results are presented. Simulations show that the robust dynamic inversion controller yields good results. |
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| Keywords: | nonlinear control robust control maneuvers |
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