期刊文献+

论惯导平台中的振动诱导漂移 被引量:5

On Vibration-Induced Drift Rate of Inertial Platform
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摘要 研究了惯导平台中的振动诱导漂移.结果表明:振动诱导漂移由常值分量和航向效应分量组成。它们的大小与陀螺转子的径向静不平衡量和轴向振动强度成正比,且与平台的结构参数、两陀螺在台体上的位置配置、两陀螺自转及轴向振动的相位移有密切关系.如不采取有效措施,将严重影响惯导系统的性能。 One of the many problems that require deeper study in present day aerospace industry in China is heading drift of inertial platform. The author applies Kayton's theory[2] to study heading drift rate, but it is believed that structural and motion parameters taken are more realistic than those of Kayton and thus the author gets results of possible use in engineering.Kayton discovered that vibration is the cause of heading drift and some other drifts. The coordinate axes used in his theoretical analysis arc fixed on the platform body. The structural and motion parameters he used arc in terms of such fixed axes and thus deviate from actual working conditions of inertial platform. The author expresses structural and motion parameters in terms of gimbal axes and thus eqs.(29 ̄32) for computing vibration-induced drift rate, including heading drift rate, is derived. Finally the author deems that effective measures, in which the findings of this paper can very likely play a part, should be taken to ensure position precision of inertial navigation through reduction of vibration-induced drift rate.
作者 郭富强
机构地区 西北工业大学
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 1995年第1期92-97,共6页 Journal of Northwestern Polytechnical University
关键词 振动诱导漂移 航向效应 惯性导航平台 vibration-induced drift, heading drift, inertial platform
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参考文献2

  • 1以光衢,惯性导航原理,1987年
  • 2刘玉峰,舰船导航,1980年,8期

同被引文献31

  • 1张伦东,潘献飞,吴美平.机抖激光陀螺检测电路前置放大器的设计与分析[J].光电子技术,2006,26(2):110-114. 被引量:7
  • 2李岷,张尧禹,李岩,于萍,时魁.基于测量船角变形光电测量系统的研究[J].长春理工大学学报(自然科学版),2006,29(3):14-15. 被引量:10
  • 3王东升,林晓彬,刘玉峰,朱玲,张宝玉.陀螺输出中的1N交流成分对平台航向效应的影响[J].中国惯性技术学报,2007,15(1):44-46. 被引量:2
  • 4陆元九.惯性器件(上、下)[M].北京:宇航出版社,1990..
  • 5江文达.航天测量船[M].北京:国防工业出版社,2002.
  • 6潘荣霖.飞航导弹惯性器件[M].北京:中国宇航出版社,1990.
  • 7潘良.航天测量船船姿船位测量技术[M].北京:国防工业出版社,2008: 2-15.
  • 8Odeberg H. Fusing sensor information using fuzzy measures[J]. Robotica, 1994, 12 (5) : 465-472.
  • 9胡平华.动力调谐陀螺稳定平台航向效应漂移研究[D].北京:中国运载火箭技术研究院,2000:50-62.
  • 10NADEAU F. The CIGTF connection : A story of precision testing at the central inertial guidance test [ C ] //Proceedings of the 51 st Annual Meeting of the Institute of Navigation( 1995 ). Ma- nassas, VA : ION, 1995:283-292.

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