| 引用本文: | 郭振云,朱伯鹏.可变落点的再入机动飞行器姿控系统设计.[J].国防科技大学学报,2004,26(3):11-14.[点击复制] |
| GUO Zhenyun,ZHU Bopeng.Attitude Control System Design of the Maneuverable Reentry Vehicle for Variable Target[J].Journal of National University of Defense Technology,2004,26(3):11-14[点击复制] |
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| 可变落点的再入机动飞行器姿控系统设计 |
| 郭振云, 朱伯鹏 |
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(国防科技大学 航天与材料工程学院，湖南 长沙 410073)
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| 摘要: |
| 基于选择的姿态反馈控制系统结构，从姿控系统稳定性能提高的角度，设计了控制系统反馈参数,以适应可变落点引起的飞行器参数变化。通过机动飞行器的六自由度飞行弹道仿真，表明所设计的姿态反馈控制系统控制效果较好，可适应预定区域内的飞行落点变化要求。 |
| 关键词: 再入机动飞行器 飞行控制 控制系统设计 姿态反馈 可变落点 飞行仿真 |
| DOI： |
| 投稿日期：2003-12-10 |
| 基金项目: |
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| Attitude Control System Design of the Maneuverable Reentry Vehicle for Variable Target |
| GUO Zhenyun, ZHU Bopeng |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| Based on the attitude feedback structure and in improvement of the system stability improving, the system feedback parameters are confirmed for adapting the flight parameters. By the simulation and analysis of six degrees of freedom, it is proved that the system can satisfiy the need of the variable target and the control effectiveness is good. |
| Keywords: maneuverable reentry vehicle flight control control system design attitude feedback variable target flight simulation |
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