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弹箭与制导学报 >

2011 , Vol. 31 >Issue 4: 1 - 4

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.04.040

导弹与制导技术

大气辅助惯导空中对准研究

  • 黎杰 ,
  • 陆志东 ,
  • 陈璞 ,
  • 张亚崇
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  • 西安飞行自动控制研究所,西安 710065

黎杰(1985-),男,湖北荆门人,硕士研究生,研究方向:组合导航。

收稿日期: 2010-11-05

  网络出版日期: 2025-05-30

基金资助

智能导航传感器导航技术研究;飞行器进近可视导航仿真与验证(2010CB731806);国家973 重点基础研究发展基金资助

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The Study of In-flight Alignment for INS Based on Air Data

  • LI Jie ,
  • LU Zhidong ,
  • CHEN Pu ,
  • ZHANG Yachong
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  • Flight Automatic Control Research Institute, Xi'an 710065, China

Received date: 2010-11-05

  Online published: 2025-05-30

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摘要

INS/GPS在进行空中对准时通常需要机体作机动以此来增强姿态误差角的可观性,由于GPS信号在机动条件下误差较大且与惯导信息的同步性不好,对准效果很差。针对以上问题,文中提出了利用大气数据系统输出的真空速辅助惯性基准系统进行三组合空中对准的方法,与传统的对准方法相比,飞机无需机动飞行,只需要匀速直线运动便可以完成空中对准,大大提高对准精度并且缩短对准时间。通过仿真,验证了以上方法的有效性。

关键词： 大气数据惯性基准系统; 大气数据; 真空速; 空中对准

本文引用格式

黎杰 , 陆志东 , 陈璞 , 张亚崇 . 大气辅助惯导空中对准研究[J]. 弹箭与制导学报, 2011 , 31(4) : 1 -4 . DOI: 10.15892/j.cnki.djzdxb.2011.04.040

Abstract

INS/GPS requires the aircraft to maneuver for better observation of the attitude errors in in-fight alignment. However, the effect of the alignment is very bad because error of GPS signal is greater and synchronization is bad when aircraft maneuvers. A method of in-flight alignment by using true air speed aid inertial reference system output by air data system was presented. Compared with the traditional alignment, aircraft needn't maneuver, the in-flight alignment can be realized by the aircraft's uniform straight motion, thereby the alignment precision is improved and the time is reduced. Simulation proves the validity of the method above.

Key words： ADIRS; air data; true air speed; in-flight alignment

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参考文献

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