| 一种测量计算飞行器初始姿态角的新方法 |
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| 引用本文： | 王庆春,杨培源.一种测量计算飞行器初始姿态角的新方法[J].宇航计测技术,2012,32(2):12-14. |
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| 作者姓名： | 王庆春 杨培源 |
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| 作者单位： | 中国人民解放军91550部队,大连,116023 |
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| 摘 要： | 根据发射平台自身特性,运用特殊点、线、面之间存在的几何关系,总结出一种简便的飞行器发射方位角和初始姿态角的测量计算方法,为飞行器参数装订提供了可靠保障。通过飞行试验验证,证明了该测量计算方法有效性。
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| 关 键 词： | 飞行器 姿态角 射向标定 测量 计算 |
A New Measurement and Calculation Method of Aircraft' s Primeval Posture |
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| WANG Qing-chun
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YANG Pei-yuan.A New Measurement and Calculation Method of Aircraft' s Primeval Posture[J].Journal of Astronautic Metrology and Measurement,2012,32(2):12-14. |
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| Authors: | WANG Qing-chun YANG Pei-yuan |
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| Institution: | 1550 Army Unit,Dalian 116023) |
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| Abstract: | According to the specific properties of the launching stand,based on the geometric relationship in particular points,lines and faces,a simple and convenient method of measurement and calculation of aircraft＇s primeval posture is concluded,providing the aircraft parameters bookbinding with reliable guarantee.The availability of this method is proved by flight tests. |
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| Keywords: | Aircraft Posture Launching direction calibration Measurement Calculation |
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