| 余度捷联惯性测量装置的优化设计研究 |
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| 引用本文： | 夏克寒,许化龙. 余度捷联惯性测量装置的优化设计研究[J]. 导弹与航天运载技术, 2005, 0(1): 6-9 |
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| 作者姓名： | 夏克寒 许化龙 |
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| 作者单位： | 第二炮兵工程学院,西安,710025;第二炮兵工程学院,西安,710025 |
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| 摘 要： | 冗余技术是改善导弹系统可靠性和精度的重要途径.为了获得导弹系统可靠性及精度与冗余度的总体优化,讨论了余度捷联惯性测量装置的优化模型及其算法,并进行了理论分析及公式推导.仿真实例也表明,模型和方法都是有效的,比较简单实用.
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| 关 键 词： | 惯性测量装置 冗余技术 优化设计 |
| 文章编号： | 1004-7182(2005)01-0006-04 |
| 修稿时间： | 2003-12-25 |
Study on Optimal Design of Redundant Strapdown Inertial Measurement Unit |
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| Xia Kehan,Xü Hualong. Study on Optimal Design of Redundant Strapdown Inertial Measurement Unit[J]. Missiles and Space Vehicles, 2005, 0(1): 6-9 |
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| Authors: | Xia Kehan Xü Hualong |
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| Abstract: | Redundant technique is an important approach of increasing the accuracy and reliability of missile. In order to obtain the optimal result, the optimal model and scheme of redundant strapdown inertial measurement unit are discussed. This paper performs a theoretical analysis of the scheme and gives a simulation. They all show that the model and algorithm are very effective. |
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| Keywords: | Inertial measurement unit Redundant technique Optimal design |
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