| 飞行器大角度机动控制实验技术研究 |
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| 引用本文： | 高桦,陈旭.飞行器大角度机动控制实验技术研究[J].实验室研究与探索,2008,27(1):22-25. |
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| 作者姓名： | 高桦 陈旭 |
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| 作者单位： | 哈尔滨工业大学航天学院,黑龙江哈尔滨,150001 |
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| 摘 要： | 讨论了空间飞行器大角度机动控制实验平台的实现方法,并给出了硬件结构原理和软件的设计流程。采用轨迹跟踪PD控制算法,设计了基于喷气系统的大角度姿态机动控制器,并进行了不同角度下的闭环姿态机动控制实验。
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| 关 键 词： | 大角度机动 喷气系统 DSP 轨迹跟踪 |
| 文章编号： | 1006-7167(2008)01-0022-04 |
| 修稿时间： | 2007年5月25日 |
Research on Experimental Technology for Spacecraft Large Angle Maneuver Control |
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| GAO Hua,CHEN Xu.Research on Experimental Technology for Spacecraft Large Angle Maneuver Control[J].Laboratory Research and Exploration,2008,27(1):22-25. |
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| Authors: | GAO Hua CHEN Xu |
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| Abstract: | This article discussed the implementation method of experimental platform for spacecraft large-angle maneuver control.The hardware structural principle and the process of software design were given out.The spacecraft large-angle maneuver controller,which is based on the gas injection system,was designed by using the control algorithm of trajectory tracking and PD control.Furthermore,the experiments of closed loop attitude maneuver control under different angles were carried out. |
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| Keywords: | large-angle maneuver gas injection system DSP trajectory tracking |
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