| 航天飞机上升与轨道过渡段制导-导航控制 |
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| 引用本文： | 张谦.航天飞机上升与轨道过渡段制导-导航控制[J].航天控制,1990(4). |
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| 作者姓名： | 张谦 |
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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： | 本文分析了航天飞机上升与轨道过渡飞行阶段的制导-导航控制装置及其分系统,并介绍了冗余系统数据选取办法。描述了四框架惯性平台框架配置与运载火箭姿态角的关系、工具误差模型与其修正方框图。最后,介绍了航天飞机制导-导航控制系统的可靠性设计。
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| 关 键 词： | 航天飞机 制导 导航 可靠性设计 ~+误差模型 冗余技术 |
GUIDANCE-NAVIGATION CONTROL OBOUT ASCENT STAGE AND ORBITAL TRANSITION STAGE OF A SHUTTLE |
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| Zhang Qian Beijing Aerospace Automatic Control Institute.GUIDANCE-NAVIGATION CONTROL OBOUT ASCENT STAGE AND ORBITAL TRANSITION STAGE OF A SHUTTLE[J].Aerospace Control,1990(4). |
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| Authors: | Zhang Qian Beijing Aerospace Automatic Control Institute |
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| Institution: | Zhang Qian Beijing Aerospace Automatic Control Institute |
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| Abstract: | This paper analyses the guidance-navigation control device with its subsystemwhich is used in the ascent stage and the orbital transition stage of a shuttle, presents a methodused to choose data for a redundant system, describes the relationship between the configura-tion of afour-gimbal inertial platform and the attitude angle of a rocket, the error model ofthe instruments and its correction block diagram. Finally, it introduces reliability design aboutthe guidance-navigation system of the shutlle. |
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| Keywords: | Shuttle Guedance Navigation Reliability design ~+Error model Redundant technology |
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