| 飞行器大姿态飞行时姿态偏差的相互转换 |
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| 引用本文： | 高玉林.飞行器大姿态飞行时姿态偏差的相互转换[J].航天控制,1992(1). |
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| 作者姓名： | 高玉林 |
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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： | 本文结合弹道式地地导弹和运载器稳定平台提供的测量角度,研究了姿控系统的姿态角、框架角和旋转角之间,尤其是各偏差之间的关系,为正确实现姿态信号反馈,特别是大姿态控制提供了依据。
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| 关 键 词： | 面对面导弹 运载火箭 姿态控制系统 |
The interconversion of attitude deviations of aerospacecraft during large attitude flight |
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| Gao yu-lin Beijing Aerospace Automatic Control Institude.The interconversion of attitude deviations of aerospacecraft during large attitude flight[J].Aerospace Control,1992(1). |
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| Authors: | Gao yu-lin Beijing Aerospace Automatic Control Institude |
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| Institution: | Gao yu-lin Beijing Aerospace Automatic Control Institude |
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| Abstract: | In this paper the research of the relations among attitude angles, frame angles and rotation angles, particularly between their deviations, is presented. Frame angles are measured from inertial stabilizing platforms mounted on in ground-to-ground ballistic missile and launch vehicle. Therefore the theoretical basis is established to implement correctlg attitude deviation feedbacks and particularly the large attitude control. |
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| Keywords: | Subject terms Ground to ground missile Launch vehicle Attitude control system |
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