| 引用本文: | 刘明俊,杨壮志,康家仁.再入机动弹头滚动回路鲁棒姿态控制系统设计.[J].国防科技大学学报,1996,18(1):40-43.[点击复制] |
| Liu Mingjun,Yang Zhuangzhi,Kang Jiaren.Reentry Warhead Roll Channel Robust Control system Design[J].Journal of National University of Defense Technology,1996,18(1):40-43[点击复制] |
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| 再入机动弹头滚动回路鲁棒姿态控制系统设计 |
| 刘明俊1, 杨壮志1, 康家仁2 |
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(1.国防科技大学;2.航天工业总公司)
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| 摘要: |
| 根据经典控制理论，引入姿态角加速度反馈, 采用零、极点相消, 变增益补偿等设计方法,所设计的再入机动弹头滚动回路姿态控制系统具有良好的快速性、稳定性和很强的鲁棒性。 |
| 关键词: 零极点相消, 控制系统设计, 鲁棒性 |
| DOI： |
| 投稿日期：1995-03-28 |
| 基金项目:国防科技预研基金资助项目 |
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| Reentry Warhead Roll Channel Robust Control system Design |
| Liu Mingjun1, Yang Zhuangzhi1, Kang Jiaren2 |
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(1.National University of Defence Technology;2.Beijing Institute of Control Instruments)
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| Abstract: |
| According to the classical control theory, this paper introduces attitude angle acceleration feedback. Using the methods of the zero and pole points cancellation, ete ., we designed reentry warhead roll channel control system with fast response speed stability and strong robustness. |
| Keywords: zero and pole point cancellation, control system design, robustness |
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