| 飞行器姿态系统变结构控制的研究 |
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| 引用本文： | 朱民雄,孙建华.飞行器姿态系统变结构控制的研究[J].宇航学报,1996,17(3):86-90. |
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| 作者姓名： | 朱民雄 孙建华 |
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| 作者单位： | 北京航空航天大学(朱民雄)，清华大学(孙建华)，中国运载火箭技术研究院(徐旭东)，中科院自动化所(叶修盛) |
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| 摘 要： | 对于具有纯延迟、惯性和由开关控制的非线性飞行器姿态系统，本文提出了采用解耦变结构控制的方法。计算机仿真结果表明，本方法行之有效，具有优良的鲁棒性，设计方法简单和易于实现数字控制等优点
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| 关 键 词： | 飞行器姿态控制系统变结构控制 |
RESEARCH ON ATTITUDE SYSTEM OF FLYING VEHICLE WITH VARIABLE STRUCTURE CONTROL |
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| Zhu Minxiong.RESEARCH ON ATTITUDE SYSTEM OF FLYING VEHICLE WITH VARIABLE STRUCTURE CONTROL[J].Journal of Astronautics,1996,17(3):86-90. |
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| Authors: | Zhu Minxiong |
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| Abstract: | For nonlinear attitude system of flying vehicle with pure time-delay, inertia and bang-bang control a control method using decoupling variable structure is given. Results of computer simulation indicate that it is effective for the method and has advantages of excellent robustness, simple design method and easily realized digital control etc. |
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| Keywords: | Flying vehicle Attitude control system Variable structure control |
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