| 反坦克导弹的一种自校正制导控制方法 |
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| 引用本文： | 刘民,康景利.反坦克导弹的一种自校正制导控制方法[J].航空学报,1994,15(5):564-569. |
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| 作者姓名： | 刘民 康景利 |
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| 作者单位： | 北京理工大学飞行器工程系 |
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| 摘 要： | 利用规范化模型和加权自校正控制方法,对反坦克导弹提出了一种自校正控制器。并在广义最小方差自校正控制律中引入了能自动调整的加权因子,以兼顾系统的稳定性和动态性能指标及适应反坦克导弹快速时变对象的控制要求。数字仿真结果表明,这种控制器对反坦克导弹有很好的控制效果,而且控制器算法简单,对过程的非线性、阶次失配和未建模扰动均有较强的鲁棒性。
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| 关 键 词： | 导弹制导 正规化 自动控制 加权函数 |
A SELF-TUNING GUIDED CONTROL METHOD OF ANTI-TANK MISSILE |
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| Liu Min,Kang Jingli.A SELF-TUNING GUIDED CONTROL METHOD OF ANTI-TANK MISSILE[J].Acta Aeronautica et Astronautica Sinica,1994,15(5):564-569. |
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| Authors: | Liu Min Kang Jingli |
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| Institution: | Dept.of Flying Vehicle Engineering of Beijing Institute of Technology,Beijing,100081 |
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| Abstract: | For anti-tank missile,this paper presents a selftuning controller by means of normal-ized model and weighting self-tuning control method.An auto-regulation weighting factor is inroduced into the generalized minimum variance self-tuning control law in order to take account of both the stability aid the dynamic index of the system and fit in with the needs of the control for the fast time-varying plant like anti-tank missile,The digital simulation shows that the controller is satisfactory for anti-tank missile.The controller has simple algorithm and stronger robustness for nonlinear,mismatched order and unmodeled disturbance of the Drocess. |
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| Keywords: | missile guidance(motion) normalizing(statlation ) automatic control weighting functions |
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