An innovative scheme for SINS/GPS ultra-tight integration system with low-grade IMU-Reference-Cited by-同舟云学术

An innovative scheme for SINS/GPS ultra-tight integration system with low-grade IMU

Published:2012-12 Issue:1 Volume:23 Page:452-460
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Xin-long,Li Ya-feng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference14 articles.

1. S. Alban, Design and performance a robust GPS/INS attitude system for automobile, PhD thesis, Stanford University, Stanford, California, USA, 2004.

2. S. Alban, D.M. Akos, S.M. Rock, Performance analysis and architectures for INS-aided GPS tracking loops, in: Institute of Navigation National Technical Meeting, ION, 2003, pp. 611–622.

3. A novel architecture for ultra-tight HSGPS-INS integration;Gao;Journal of Global Positioning System,2008

4. J.D. Gautier, GPS/INS generalized evaluation tool (GIGET) for the design and testing of integrated navigation systems, PhD thesis, Stanford University, Stanford, California, USA, 2003.

5. Sensitivity and performance analysis of Doppler-aided GPS carrier-tracking loops;Gebre-Egziabher;Navigation: Journal of the Institute of Navigation,2005

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