| 导弹姿态控制系统的全程模糊滑模控制设计与仿真 |
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| 引用本文： | 米文鹏,洪成华,杨建飞.导弹姿态控制系统的全程模糊滑模控制设计与仿真[J].兵工自动化,2008,27(9):14-15. |
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| 作者姓名： | 米文鹏 洪成华 杨建飞 |
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| 作者单位： | 1. 第二炮兵工程学院,603,教研室,陕西,西安,710025
2. 第二炮兵青州士官学校,103,教研室,山东,青州,262500 |
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| 摘 要： | 结合模糊控制器和变结构控制器的各自优点，给出导弹姿态控制系统的模糊滑模控制，同时为消除模糊滑模控制的能达阶段，在控制器中引入全程滑模因子，最终实现导弹姿态控制系统的全程模糊滑模控制，取得了较好的效果。
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| 关 键 词： | 模糊滑模控制 全程滑模变结构控制 姿态控制系统 全程滑模因子 |
Global FVSC Design and Simulation for Missile Attitude-Control System |
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| MI Wen-peng,HONG Cheng-hua,YANG Jian-fei.Global FVSC Design and Simulation for Missile Attitude-Control System[J].Ordnance Industry Automation,2008,27(9):14-15. |
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| Authors: | MI Wen-peng HONG Cheng-hua YANG Jian-fei |
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| Affiliation: | MI Wen-peng, HONG Cheng-hua, YANG Jian-fei (1. No. 603 Staff Room, The Second Artillery Engineering College, Xi＇an 710025, China; 2. No. 103 Staff Room, Qingzhou Petty Officer School of the Second Artillery, Qingzhou 262500, China) |
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| Abstract: | Based on the advantages of fuzzy controller and variable structure controller (VSC), design the fuzzy variable structure controller (FVSC) for missile attitude-control system, and adopt the global sliding gene to eliminate the reaching interval of the controller. At last, realize global FVSC of missile attitude-control system. The results show that the missile attitude-control system based on global FVSC has global robustness and good effect. |
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| Keywords: | FVSC Global VSC Attitude-control system Global sliding gene |
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