| 可重复使用运载器的工程化姿态控制系统设计 |
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| 引用本文： | 钱山,刘新建,佟卫平,蔡洪. 可重复使用运载器的工程化姿态控制系统设计[J]. 弹箭与制导学报, 2009, 29(5) |
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| 作者姓名： | 钱山 刘新建 佟卫平 蔡洪 |
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| 作者单位： | 1. 国防科技大学航天与材料工程学院,长沙,410073
2. 北京航天自动控制研究所,北京,100854 |
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| 基金项目： | 教育部新世纪优秀人才支持计划 |
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| 摘 要： | 基于古典控制理论和BTT倾斜转弯控制技术,设计了可重复使用运载器(RLV)的大气层内姿态稳定控制系统.控制系统采用角速率和加速度作为PI控制的反馈信号,系统实现简单,可同时满足侧向大、小扰动情况下的姿态稳定控制要求.数值仿真结果表明该方案有效可行.
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| 关 键 词： | 倾斜转弯 可重复使用运载器 姿态控制 |
Engineering Attitude Control System Design of Reusable Launch Vehicle |
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| QIAN Shan,LIU Xinjian,TONG Weiping,CAI Hong. Engineering Attitude Control System Design of Reusable Launch Vehicle[J]. Journal of Projectiles Rockets Missiles and Guidance, 2009, 29(5) |
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| Authors: | QIAN Shan LIU Xinjian TONG Weiping CAI Hong |
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| Affiliation: | QIAN Shan1,LIU Xinjian1,TONG Weiping2,CAI Hong1(1 College of Aerospace & Material Engineering,National University of Defense Technology,Changsha 410073,China,2 Beijing Aerospace Automatic Control Institute,Beijing 100854,China) |
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| Abstract: | Focused on the problem of reusable launch vehicle(RLV) attitude control,an engineering attitude control system based on the classical control theory and BTT technology was designed.The angular rate and the acceleration were used as feedback signals controlled by the PI.Then,the mentioned attitude control system was applied to the condition of large/small side perturbation.The simulation results show that the proposed control system is easy to be implemented and has good engineering applicability because all... |
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| Keywords: | BTT reusable launch vehicle attitude control |
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