| 导弹纵向机动飞行的非线性鲁棒控制研究 |
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| 引用本文： | 查旭,崔平远,刘永才.导弹纵向机动飞行的非线性鲁棒控制研究[J].飞行力学,2004,22(1):56-59. |
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| 作者姓名： | 查旭 崔平远 刘永才 |
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| 作者单位： | 1. 哈尔滨工业大学,航天工程与力学系,黑龙江,哈尔滨,150001
2. 中国航天科工集团,第三研究院,北京,100074 |
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| 摘 要： | 将非线性无源方法用于导弹纵向机动飞行控制，并通过变结构控制器补偿系统的不确定性，这样设计的控制器能保证系统的鲁棒稳定性。将此方法用于导弹地形跟踪控制，仿真结果表明：此方法在导弹纵向机动飞行中控制效果较好。
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| 关 键 词： | 导弹 纵向机动飞行 非线性鲁棒控制 地形跟踪控制 变结构控制器 |
| 文章编号： | 1002-0853(2004)01-0056-04 |
| 修稿时间： | 2003年3月25日 |
A Study of Nonlinear Robust Control of Longitudinal Maneuvering Flight for Missiles |
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| ZHA Xu,CUI Ping-yuan,LIU Yong-cai.A Study of Nonlinear Robust Control of Longitudinal Maneuvering Flight for Missiles[J].Flight Dynamics,2004,22(1):56-59. |
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| Authors: | ZHA Xu CUI Ping-yuan LIU Yong-cai |
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| Institution: | ZHA Xu~1,CUI Ping-yuan~1,LIU Yong-cai~2 |
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| Abstract: | In this paper, the passivity-based control method is applied to the missile longitudinal maneuvering flight control and the compensatory controller is designed using the variable structure control techniques which deal with uncertainties of a system. The method ensures robust stability of the control system.The control laws are used in terrain following. The simulation results show that the control laws have better for missiles during longitudinal maneuvering flight conditions. |
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| Keywords: | passivity method variable structure control flight control missile |
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