Performance analysis of a tightly coupled Kalman filter for the integration of un-differenced GPS and inertial data

Proceedings of the Institute of Navigation, National Technical Meeting

Volumn , Issue , 2005, Pages 270-275

  Zhang, Yufeng ^a   Gao, Yang ^a,b  

^a UNIVERSITY OF CALGARY   (Canada)

^b International Association of Geodesy's Sub Commission 45: Next Generation RTK

Author keywords

[No Author keywords available]

Indexed keywords

CLOCK ERRORS; INERTIAL SENSORS; PERFORMANCE ANALYSIS; PRECISE POINT POSITIONING (PPP);

DEGREES OF FREEDOM (MECHANICS); INERTIAL NAVIGATION SYSTEMS; KALMAN FILTERING; NAVIGATION; PERFORMANCE; POSITION MEASUREMENT; RELIABILITY; TRAJECTORIES;

GLOBAL POSITIONING SYSTEM;

EID: 27744534344     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Zhang, Y, and Gao, Y (2004). "Design and Analysis of a Tightly Coupled Kalman Filter for a Point GPS/INS System: Preliminary Results", Proceedings of 2004 International Symposium on GPS/GNSS, Sydney, Australia, November 6-8, 2004.
2. Gao, Y, and Shen, X (2002). "A New Method for Carrier-Phase-Based Precise Point Positioning", Navigation, Journal of The Institute of Navigation, 49(2): 109-116.
3. Muellerschoen. RJ, Bar-Sever, YE, Bertiger, WI and Stowers, DA (2001). "NASA's Global DGPS for High Precision Users", GPS World, 12(1): 14-20.
4. Petovello, M, Cannon, ME, and Lachapelle, G (2004). "Benefits of Using a Tactical-Grade IMU for High-Accuracy Positioning", Navigation, Journal of The Institute of Navigation, 51(1): 1-12.
5. Parkinson, BW, Spilker, JJ (1996). Global Positioning System: Theory and Applications, American Institute of Aeronautics.