| 卫星用飞轮状态反馈控制技术 |
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| 引用本文： | 胡玉琛,赵洪峰.卫星用飞轮状态反馈控制技术[J].宇航学报,1992(4):1-8. |
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| 作者姓名： | 胡玉琛 赵洪峰 |
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| 作者单位： | 北京控制工程研究所 100080
(胡玉琛，赵洪峰)，北京控制工程研究所 100080(唐铮) |
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| 摘 要： |
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| 关 键 词： | 状态反馈 卡尔曼滤波 卫星 |
THE CONTROL TECHNOLOGY OF WHEEL STATE FEEDBACK IN THE SATELLITE |
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| Hu Yuchen Zhao Hongfeng Tang Zheng.THE CONTROL TECHNOLOGY OF WHEEL STATE FEEDBACK IN THE SATELLITE[J].Journal of Astronautics,1992(4):1-8. |
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| Authors: | Hu Yuchen Zhao Hongfeng Tang Zheng |
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| Abstract: | The control, technology of wheel state feedback is the. leading topic of the actuator in the satellite attitude control system. Based on the theoretical analysis. Computer simulation and engineering model experiment, it has been proved that the bad influence of internal disturbance torgue to satelite control system can be reduced by the use of wheel state feedback and Kalman filter theory. The methods in this paper have been supplied for raising the precision of satellite attitude control system and reducing satellite board's jitter. |
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| Keywords: | State feedback Internal disturbance torgue Noise reduction Kal-man filtering |
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