| 直升机超视距主动引导定位分析 |
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| 引用本文： | 黄志宇,徐清华,谢国新,刘钢.直升机超视距主动引导定位分析[J].舰船电子工程,2007,27(1):58-59. |
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| 作者姓名： | 黄志宇 徐清华 谢国新 刘钢 |
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| 作者单位： | 海军兵种指挥学院,广州,510430 |
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| 摘 要： | 针对直升机成为超视距导弹攻击引导兵力的需求,对直升机超视距引导定位方法及解算模型进行探讨,采用大地主题正反解方法,建立惯导大地法、航姿大地法、双向定位法三种不同引导定位方法的定位解算模型,并编程进行模型解算,为舰载反舰导弹进行精确超视距导弹攻击提供引导保障。
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| 关 键 词： | 超视距 惯导大地法 航姿大地法 双向定位法 |
| 修稿时间： | 2006年6月14日 |
Analysis on the Positioning of Helicopter OTH Active - guiding |
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| Huang Zhiyu.Analysis on the Positioning of Helicopter OTH Active - guiding[J].Ship Electronic Engineering,2007,27(1):58-59. |
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| Authors: | Huang Zhiyu |
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| Institution: | Huang Zhiyu |
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| Abstract: | In this paper, the positioning method and calculating model of the helicopter OTH active-guiding are discussed in light of the requirement that helicopter be the guiding force of OTH missile attack ,direct/inverse solution of geodetic problem is used and the positioning calculating models of three different methods including Inertia-navigation,Navigation-pose and Bi-orientation of guiding-position are created. Finally a procedure is produced to calculate these models,it provides guiding guarantee for shipborne SSM OTH attack. |
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| Keywords: | OTH inertia-navigation navigation-pose Bi-orientation of guiding-position |
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