| 飞航导弹块对角模型组合控制算法的仿真 |
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| 引用本文： | 吴光彬,胡云安. 飞航导弹块对角模型组合控制算法的仿真[J]. 系统仿真学报, 2001, 13(2): 168-170 |
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| 作者姓名： | 吴光彬 胡云安 |
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| 作者单位： | 海军航空工程学院自动控制工程系, |
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| 摘 要： | 飞航导弹的运动模型可以表示成一种四层块对角结构,对基于导弹块对角模型的组合控制算法进行了仿真,结果表明,对导弹这样一个高时变非线性系统,采用组合控制算法较之解析逆解算法和变结构控制算法具有更好的鲁棒性。
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| 关 键 词： | 飞航导弹 块对角 组合控制算法 仿真 |
| 文章编号： | 1004-731X(2001)02-0168-03 |
| 修稿时间： | 1999-11-18 |
The Combined ControlArithmetic Simulation of Missile's Block Diagonal System |
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| WU Guang-bin,HU Yun-an. The Combined ControlArithmetic Simulation of Missile's Block Diagonal System[J]. Journal of System Simulation, 2001, 13(2): 168-170 |
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| Authors: | WU Guang-bin HU Yun-an |
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| Abstract: | A guided missile's model can be expressed as four layers of Block Diagonal System. The combined control arithmetic simulation of a missile's Block Diagonal System is described. The simulation results have shown that the given algorithm has advantages such as high Robustness and dynamic performances over inverse resolution or variable structure control algorithm for the high-order, time-varying, non-linear missile control system. |
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