Technology research of ultra-tightly integration about INS aided tracking loop based on EKF-Reference-Cited by-同舟云学术

Technology research of ultra-tightly integration about INS aided tracking loop based on EKF

Published:2016 Issue: Volume: Page:
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Container-title:Proceedings of the 2016 International Conference on Intelligent Information Processing - ICIIP '16
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Author:

Huang Xun¹,Zhan Jinlin¹,Zhang Yuan¹

Affiliation:

1. Naval Petty Officer Academy, An Hui, China

Publisher

ACM Press

Reference8 articles.

1. Gautier J. D, B. W. Parkinson. 2003. Using the GPS/INS Generalized evaluation Tool (GIGET) for the Comparison of Loosely Coupled, Tightly Coupled and Ultra-Tightly Coupled Integrated Navigation Systems. Inproceedings of ION 59th Annual Meeting/CIGTF 22nd Guidance Test Symposium(Albuquerque, June 23--25, 2003). NM, Institute of Navigation, Fairfax VA, 65--76.

2. Guojiang G. 2007.INS-Assisted High Sensitivity GPS Receivers for Degraded Signal Navigation.Doctoral Thesis. UCGE Reports Number: No.20252 The University of Calgary.

3. Babu, R., Wang, J. 2009. Ultra-tight GPS/INS/PL integration: a system concept and performance analysis.GPS solutions, (Jan. 2009), 75--82.

4. Wang, X. L., Li, Y. F. 2012. An innovative scheme for SINS/GPS ultra-tight integration system with low-grade IMU. Aerospace Science and Technology, (Jan. 2012), 452--460.

5. Beser, J. 2002. Trunav: A Low Cost Guidance/Navigation Unit Integrating a SAASM Based GPS and MEMS in Deeply Coupled Mechanization.The Institute of Navigation ION-GPS(Portland, USA, 2003), 24--27.

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