An improved tightly coupled approach for GPS/INS integration

2004 IEEE Conference on Robotics, Automation and Mechatronics

Volumn , Issue , 2004, Pages 1164-1167

  Wang, Wei ^a   Liu, Zongyu ^a   Xie, Rongrong ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; AIRCRAFT; COMPUTER SIMULATION; ERROR ANALYSIS; KALMAN FILTERING; LINEAR EQUATIONS; MARKOV PROCESSES; MATRIX ALGEBRA; PERTURBATION TECHNIQUES; SATELLITES; ALGORITHMS; INERTIAL NAVIGATION SYSTEMS; LINEARIZATION; PROBLEM SOLVING; SENSORS; STABILITY;

AIRCRAFT TRAJECTORY; HESSIAN MATRIX; INERTIAL NAVIGATION SYSTEM (INS); LINEAR FILTERS; DATA UPDATE RATE; ERROR MODELS; INERTIAL DEVICES; SHORT TERM STABILITY;

GLOBAL POSITIONING SYSTEM;

EID: 11244306805     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

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2. Kaplan, E. D. Understanding GPS, Principle and Applications. Boston: Artech House, 1996.
3. Xuan Xin, Yu Jixiang and Chen Zhe. Navigation System. Beijing: Aviation Industry Press, 1993 (In Chinese).
4. Wei, M., and Schwarz, K. P. A discussion of models for GPS/INS integration. In Y. Bock and N. Leppard (Eds.), Global Positioning Systems: An Overview. New York: Springer-Verlag, 1989, pp.314-327.
5. Jörg F. Wagner, Thomas Wieneke. "Integrating satellite and inertial navigation - conventional and new fusion approaches," Control Engineering Practice, 11 (2003): pp.543-550.
6. G. Arshal, "Error Equations of Inertial Systems," Journal of Guidance, Navigation and Dynamics, Vol.10, No.4, pp. 351-358, 1987.
7. LeMaster E.A. Self-Calibrating Pseudolite Arrays: Theory and Experiment, Ph.D. Thesis, Stanford University, 2002.