[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2017 , Vol. 37 >Issue 4: 9 - 13

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2017.04.003

MISSILES AND GUIDANCE TECHNOLOGY

SINS/SRS Autonomous Integrated Navigation System Design

  • GAO Zhaohui ,
  • MU Dejun ,
  • WEI Wenhui ,
  • GAO Shes heng ,
  • ZHANG Jing
Expand
  • School of Automation, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2017-03-16

  Online published: 2025-05-28

Fold

Abstract

In order to meet the requirements of cruise missile for high precision and high reliability of navigation system, a new methods for strap-down inertial navigation (SINS) /spectral redshift (SRS) autonomous integrated navigation based on the principles of the spectral redshift velocity measurement was presented. On the basis of studying the principle of spectral redshift navigation, the scheme of SINS/SRS autonomous integrated navigation system was designed, and the mathematical model and algorithm of the integrated navigation system were established, and the simulation was carried out. The results showed that the proposed new method for SINS/SRS autonomous integrated navigation could adjust SINS by using the high precision velocity information obtained by adopting SRS and effectively restrain the error of SINS accumulating over time. And the method had high precision and good reliability, and could meet the requirements of cruise missile for navigation system performance.

Key words： spectral redshift; strap-down inertial navigation; SINS/SRS integrated navigation

Cite this article

GAO Zhaohui , MU Dejun , WEI Wenhui , GAO Shes heng , ZHANG Jing . SINS/SRS Autonomous Integrated Navigation System Design[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(4) : 9 -13 . DOI: 10.15892/j.cnki.djzdxb.2017.04.003

[an error occurred while processing this directive]

References

[1]
王永, 赵剡, 杨奎. 基于小波分析和密度估计的红移测速导航研究[J]. 航空兵器, 2014(6):37-41.
[2]
张伟, 陈晓, 尤伟,等. 光谱红移自主导航新方法[J]. 上海航天, 2013, 30(2):32-33.
[3]
张剑峰. 地磁/光谱红移组合导航系统研究[D]. 哈尔滨: 哈尔滨工业大学, 2014:9-24.
[4]
高社生, 何鹏举, 杨波,等. 组合导航原理及应用[M]. 西安: 西北工业大学出版社, 2012:121-422.
[5]
HUGGINS W. Further observations on the spectra of some of stars and nebulae, with an attempt to determine therefrom whether these bodies are moving towards or from earth, also observations on the spectra of the sun and of comet II, 1868[J]. Philosophical Transactions of the Royal Society of London, 1942, 158(6):529-564.
[6]
TONRY J, DAVIS M. A survey of galaxy redsgifts. I. data reduction techniques[J]. The Astronomical Journal, 1979, 84(10):1511-1525.
[7]
HU Gaoge, GAO Shesheng, ZHONG Yongmin, et al. Modified federated Kalman filter for INS/GNSS/CNS integration[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 230(1):30-44.
[8]
ZHONG Yongmin, GAO Shesheng, LI Wei. A quaternion-based method for SINS/SAR integrated navigation system[J]. IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(1):514-524.
[9]
GAO Zhaohui, MU Dejun, GAO Shesheng, et al. Robust adaptive filter allowing systematic model errors for transfer alignment[J]. Aerospace Science and Technology, 2016, 59:32-40.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]