| 飞行器变结构姿态控制的研究 |
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| 引用本文： | 陈宏钧,王卓军.飞行器变结构姿态控制的研究[J].哈尔滨工业大学学报,1997,29(6):11-13. |
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| 作者姓名： | 陈宏钧 王卓军 |
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| 作者单位： | 哈尔滨工业大学电气工程系 |
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| 基金项目： | 国家863计划409主题资助项目 |
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| 摘 要： | 本文针地飞行器姿态控制中存在的子系统之间的动态耦合问题，给出了一种自适应变结构控制律。并对于变结构控制中存在的模态颤振问题提出了一种具体解决方法。理论分析和仿真研究表明此控制律具有姿态跟踪精度高，实时计算量小，便于工程实现等优点。
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| 关 键 词： | 空间拦截 姿态控制 变结构控制 飞行器 |
Research on Variable Structure Attitude Control of Aircraft |
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| Chen Hongjun,Wang Zhuojun,Zhou Di,Hu Hengzhang.Research on Variable Structure Attitude Control of Aircraft[J].Journal of Harbin Institute of Technology,1997,29(6):11-13. |
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| Authors: | Chen Hongjun Wang Zhuojun Zhou Di Hu Hengzhang |
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| Affiliation: | Dept.of Control Engineering |
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| Abstract: | This paper presents a kind of adaptive variable structure control law for the dynamic coupling problems existing between subsystems of the aircraft attitude control and discusses a method to solve the sliding mode vibration problem in the variable structure control system.Theoretical analysis and the simulation results show that this method has the advantages of good attitude tracking accuracy,less real time calculations and easy realization. |
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| Keywords: | space interception attitude control variable structure control |
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