| 一类大机动导弹的非线性控制问题 |
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| 引用本文： | 陈德源, 姚郁.一类大机动导弹的非线性控制问题[J].系统工程与电子技术,1995(7). |
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| 作者姓名： | 陈德源 姚郁 |
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| 作者单位： | 航天工业总公司二院二部，哈尔滨工业大学 |
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| 摘 要： | 本文研究了大机动飞行情况下飞行器姿态控制系统的设计问题。首先，基于非线性系统输出解耦控制的设计思想，重点解决了一类既有姿态角控制要求，又有弹道设计要求的控制系统设计问题，设计得到一种复合控制规律。最后，通过数值仿真验证了该方法的有效性。
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| 关 键 词： | 非线性控制，￣＋解耦控制，机动飞行控制。 |
Nonlinear Control Problem for a C1ass of the Great Maneuver Missiles |
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| Chen Deyuan.Nonlinear Control Problem for a C1ass of the Great Maneuver Missiles[J].System Engineering and Electronics,1995(7). |
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| Authors: | Chen Deyuan |
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| Abstract: | This paper studies a design problem of the vehicle attitude control system. First of all,basing on the design thinking of the nonlinear system output decouple control. the writer lays emphasis on resolving such a control system design problem which involves both attitude control requirement and trajectory design requirement,moreover has designed and obtained a kind of com-plex control rule. Finally,the validity of this design method is proven by nuinerical simulatioth |
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| Keywords: | Nonlinear system Decouple control Great maneuver flight control |
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