| 非线性系统部分线性化及其在飞行控制中的应用 |
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| 引用本文： | 姚郁,王子才.非线性系统部分线性化及其在飞行控制中的应用[J].航天控制,1991(4). |
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| 作者姓名： | 姚郁 王子才 |
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| 作者单位： | 哈尔滨工业大学，哈尔滨工业大学 |
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| 摘 要： | 本文借鉴非线性系统线性化的设计思想,提出并研究了非线性系统部分线性化问题,给出了可以对非线性系统进行部分线性化的充分必要条件。在此基础上,研究了某飞行器姿态控制系统设计问题。给出了飞行控制规律,最后通过数值仿真验证了本文提出方法的正确性。
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| 关 键 词： | 非线性系统 飞行控制系统 制导 稳定性 |
Nonlinear system partial linearization and its application to flight control |
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| Yao Yu Wang Zicai Harbin Institute of Technology.Nonlinear system partial linearization and its application to flight control[J].Aerospace Control,1991(4). |
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| Authors: | Yao Yu Wang Zicai Harbin Institute of Technology |
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| Institution: | Yao Yu Wang Zicai Harbin Institute of Technology |
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| Abstract: | The paper presents and researchs the problem of partial linearization of anonlinear system based on the design concept of lineatization of nonlinear system.The suffi-cient and necessary condition that a nonline system can partially be linearized is given.On thebase,the design problem of the attitude control system of a certain vehicle is researched and itscontrol law is given out.Finally,the correctness of the method presented in this paper is veri-fied by nvmerieal value simulation. |
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| Keywords: | Nonlinear system Flight control system Guidance Sability |
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