Nonlinear μ flight control and suboptimal exact solution on F-16 application

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作者：
Department of Aeronautical Engineering, National Defense University, Chung Cheng Institute of Technology, Taoyuan 335, Taiwan [1 ]
不详 [2 ]
不详 [3 ]
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| 1600年 / 666-671卷 / 2005期
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Compendex;
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摘要：
Flight dynamics - Gain control - Parameter estimation - Partial differential equations - Uncertain systems
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