| 远程飞航导弹的非线性控制系统设计 |
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| 引用本文： | 顾文锦,王士星,韦峰.远程飞航导弹的非线性控制系统设计[J].宇航学报,1999,20(2):28-35. |
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| 作者姓名： | 顾文锦 王士星 韦峰 |
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| 作者单位： | 海军航空工程学院,烟台,264001 |
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| 摘 要： | 本文首先根据两个原则，把远程飞航导弹非线性运动模型处理成一种块对角结构，并由此定义了块对角非线性系统和它的逆解。然后提出了一种由逆解所组成的块对角控制器的设计方法。接着，本文对远程飞航导弹进行了块对角控制器设计，取得了成功。通过仿真表明，该方法设计的系统具有良好的性能，而且有着广泛的应用潜能。
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| 关 键 词： | 远程 飞航导弹 数学模型 逆解 非线性控制系统 |
| 修稿时间： | :1997年3月17 |
A DESIGN OF NONLINEAR CONTROL SYSTEM FOR LONG-DISTANCE AERODYNAMIC MISSILE |
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| Gu Wenjin,Wang Shixing,Wei Feng.A DESIGN OF NONLINEAR CONTROL SYSTEM FOR LONG-DISTANCE AERODYNAMIC MISSILE[J].Journal of Astronautics,1999,20(2):28-35. |
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| Authors: | Gu Wenjin Wang Shixing Wei Feng |
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| Abstract: | In this paper,the motion equations of a long di stance aerodynamic missile can be transformed in block diagonal form by using gi ven two principles.Thus,a definition of block diagonal nonlinear system and its i nverse solution are proposed.After that,a design method that is called block dia gonal controller(BDC) is proposed.Therefore,a flight control system is designed using BDC's method for a long distance aerodynamic missile.The result of the de sign has been proved by mathematical simulation,which shows that the BDC's desig n has well prospects. |
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| Keywords: | Long distance aerodynamic missile\ Mathematical model for missile\ Inverse solution of model\ Nonlinear control system\ Block di agonal controller |
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