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惯性仪表误差补偿技术在提高战略导弹精度中的应用 被引量:3

Application of Error compensation Technology of Inertial Instruments in Improvement of Strategic Ballistic Missile Accuracy
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摘要 本文对有关战略导弹惯性仪表主要误差源的分类及对精度的影响;惯性仪表误差补偿的各种方法及其优缺点等内容作了介绍,对美国洲际导弹误差补偿方法也作了介绍,最后对惯性仪表误差的几种补偿方案作了分析。 In this paper,classification of the inertial instrument primary error sources of strategic missile and their influences on accuracy,as well as various methods of error compensation and advantages or shortages of them are presented.Methods used in U.S.A for intercontinental ballistic missille are also introduced.Finally,several inertial instrument error compensation shemes are analyzed.
作者 朱振乾
出处 《航天控制》 CSCD 北大核心 1995年第3期1-9,共9页 Aerospace Control
关键词 制导精度 误差补偿 战略导弹 惯性仪表 Guidance Guidance accuracy Guidance error compensation
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  • 1李广辉,张兴会,麦继平.小波变换在陀螺信号去噪中的应用[J].仪器仪表学报,2005,26(z2):506-507. 被引量:5
  • 2李莉,任长明.旋转方位惯性导航系统的研究[J].天津工程师范学院学报,2005,15(2):39-41. 被引量:4
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  • 7GAO W, CAO B, BEN Y Y, et al. Analysis of gyro's slope drift affecting inertial navigation system error [ C ]. Proceedings of the IEEE International Conference on Mechatronics and Automation, Changchun, China, 2009 : 3757-3768.
  • 8SAVAGE P G. Analytical modeling of sensor quantization in strapdown inertial navigation error equations [ J ]. Journal of Guidance, Control, and Dynamics, 2002, 25 (5) : 833 -842.
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