| 最优鲁棒控制在飞行器设计中的应用 |
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| 引用本文： | 倪茂林 王子才. 最优鲁棒控制在飞行器设计中的应用[J]. 宇航学报, 1990, 0(3): 23-27 |
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| 作者姓名： | 倪茂林 王子才 |
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| 作者单位： | 北京控制工程研究所(倪茂林)，哈尔滨工业大学(王子才) |
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| 摘 要： | 本文根据线性最优调节器加权阵与闭环系统极点的关系,提出了一种综合最优系统设计法,使系统同时具有良好的动特性和较强的鲁棒性。文中应用这种方法对某型飞行器控制系统进行了设计,使飞行器性能指标得到了显著提高。
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| 关 键 词： | 导弹 鲁棒控制 最优调节器 设计 |
THE APPLICATION OF OPTIMAL ROBUST CONTROL IN CONTROL SYSTEM DESIGN OF FLYING VEHICLES |
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| Ni Maolin. THE APPLICATION OF OPTIMAL ROBUST CONTROL IN CONTROL SYSTEM DESIGN OF FLYING VEHICLES[J]. Journal of Astronautics, 1990, 0(3): 23-27 |
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| Authors: | Ni Maolin |
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| Affiliation: | Ni Maolin(Beijing Institute of Control Engineering)Wang Zicai (Harbin Institute of Technology) |
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| Abstract: | In this paper, based on the relation between the weighting matrices in linear quadratic optimal regulator and closed loop poles, a combined design method is presented for the optimal system with excellent dynamical characteristics and robustness. Applying this method in the design of control system of a certain flying vehicle,the performance is significantly improved. |
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| Keywords: | Optimal regulator Robust control Integrity. |
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