| 一种全姿态平台实现方法的数学依据 |
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| 引用本文： | 戴邵武,王家鑫,喻楚兵.一种全姿态平台实现方法的数学依据[J].海军航空工程学院学报,2004,19(5):527-529. |
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| 作者姓名： | 戴邵武 王家鑫 喻楚兵 |
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| 作者单位： | 海军航空工程学院自动控制系,烟台,264001;海军装备部驻上海军事代表局,上海,200072 |
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| 摘 要： | 阐明了当载体做大机动飞行时,在某个方位的旋转角度过大,三环式平台便会出现闭锁现象。针对这一现象,提出了增加一个外环来实现全姿态平台的方法并提供了这种实现方法的数学依据。
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| 关 键 词： | 全姿态平台 四元数 惯性导航 |
| 修稿时间： | 2003年11月23 |
Mathematics Proof of a Realization of Full Degree Platform |
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| DAI Shao-wu,WANG Jia-xin,YU Chu-bing.Mathematics Proof of a Realization of Full Degree Platform[J].Journal of Naval Aeronautical Engineering Institute,2004,19(5):527-529. |
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| Authors: | DAI Shao-wu WANG Jia-xin YU Chu-bing |
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| Institution: | DAI Shao-wu YU Chu-bing Department of Automatic Control Engineering,NAEI,Yantai,264001,WANG Jia-xin Minitary Representatives Office of NED in Shanghai,Shanghai,200072 |
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| Abstract: | The paper illustrates that if the aircraft has a large mechanomotive,with a too much big rotatation angle in a orientation,lock-up will occur in tri-circled platform.In order to solve the problem,a idea that adding a outer circle to the tri-circled platform system consists of the full-orientation platform is put forward in the book,and mathematics proof of the idea is offered in this paper. |
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| Keywords: | full-orientation platform quatemion inertia navigation |
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