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捷联惯导系统最简多位置解析对准

谭彩铭 王宇 苏岩 朱欣华

谭彩铭, 王宇, 苏岩, 等 . 捷联惯导系统最简多位置解析对准[J]. 北京航空航天大学学报, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033
引用本文: 谭彩铭, 王宇, 苏岩, 等 . 捷联惯导系统最简多位置解析对准[J]. 北京航空航天大学学报, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033
TAN Caiming, WANG Yu, SU Yan, et al. The simplest multi-position analytic alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033(in Chinese)
Citation: TAN Caiming, WANG Yu, SU Yan, et al. The simplest multi-position analytic alignment for SINS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(9): 1645-1650. doi: 10.13700/j.bh.1001-5965.2015.0033(in Chinese)

捷联惯导系统最简多位置解析对准

doi: 10.13700/j.bh.1001-5965.2015.0033
基金项目: 国家自然科学基金青年科学基金(61301021)
详细信息
    作者简介:

    谭彩铭(1987—),男,江苏句容人,博士研究生,tancm314@hotmail.com

    通讯作者:

    苏岩(1967—),男,江苏苏州人,教授,suyan@mail.njust.edu.cn,主要研究方向为MEMS传感技术.

  • 中图分类号: U666.1

The simplest multi-position analytic alignment for SINS

  • 摘要: 传统的多位置解析对准方法一般要求将捷联惯导系统(SINS)安装在一个伺服平台上并绕天向轴旋转90°或180°,这对工程带来不便,且伺服平台的精度会影响多位置解析对准的精度.针对这一问题,提出最简多位置解析对准方法,指出任意两位置是实现SINS多位置解析对准所需的最小条件,即通常理论上任意两位置可解算出惯性测量单元(IMU)的常值偏置,给出了计算方法,并通过仿真实例加以说明和验证,可以作为一种简易初始对准或现场标定方法.另外通过解析方法指出在特殊姿态下,某单一轴向的加速度计常值偏置或陀螺常值漂移可以直接被较好地估计出来,结论可用于进一步改进多位置对准方法.

     

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出版历程
  • 收稿日期:  2015-01-19
  • 网络出版日期:  2015-09-20

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