| 姿态控制系统干扰的补偿和测量方法 |
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| 引用本文： | 王贵斌.姿态控制系统干扰的补偿和测量方法[J].航天控制,1993(4). |
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| 作者姓名： | 王贵斌 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 本文根据系统完全补偿条件,证明了弹体姿态运动俯仰和偏航通道不能对干扰完全补偿,而滚动通道则能完全补偿。文中叙述了俯仰通道非完全补偿的方法,并提出克服伺服系统动态特性对补偿影响的设想。讨论了用冲角表、角加速度计和观测器测量干扰的方法。还阐述了采用反馈实现干扰静态补偿的方法。
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| 关 键 词： | 姿态控制系统 干扰 测量 补偿 |
The Method of Interference Compensation and Measurement for the Attitude Control System |
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| Wang Guibin Beijing Aerospace Automatic Control Institute.The Method of Interference Compensation and Measurement for the Attitude Control System[J].Aerospace Control,1993(4). |
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| Authors: | Wang Guibin Beijing Aerospace Automatic Control Institute |
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| Institution: | Wang Guibin Beijing Aerospace Automatic Control Institute |
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| Abstract: | According to the complete compensation conditions of the system, this paper is to prove that the pitch and yaw channel of the missile body attitude motion can't compensate completely the interferences, but can do it for the roll channel. This paper relates the complete compensation method for the pitch channel, and puts forward an idea of overcoming the in fluences of the dynamic characteristics of servo system for the compensation. We also discuss the inter ference measuring method using the meter of attack angle, angular accelermeter and observer, as well the method of using feedback to realize the static inter ference compensation. |
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| Keywords: | Attitude control system Interference Measurement Compensation |
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