Analysis of an upgraded GPS internal Kalman filter

IEEE Aerospace and Electronic Systems Magazine

Volumn 11, Issue 1, 1996, Pages 23-26

  Weiss, J David ^a,b  

^a GENERAL DYNAMICS   (United States)

^b NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; ERRORS; GEOMETRY; GLOBAL POSITIONING SYSTEM; INERTIAL NAVIGATION SYSTEMS; MATHEMATICAL MODELS; OPTIMIZATION; POSITION MEASUREMENT; SYSTEMS ANALYSIS; VELOCITY MEASUREMENT;

ACCELEROMETER BIAS ERRORS; ATTITUDE ERROR STATES; GYRO; PRECISE POSITIONING SERVICE; TILT;

KALMAN FILTERING;

EID: 3343002241     PISSN: 08858985     EISSN: None     Source Type: Journal    
DOI: 10.1109/62.484146     Document Type: Article

References (1)

1. Weiss, J. D. and Kee, D. S., June 5-7, 1995, "A Direct Performance Comparison Between Loosely Coupled & Tightly Coupled GPS/INS Integration Techniques," Institute of Navigation, Proceedings of the 51st Annual Meeting, Colorado Springs, Colorado, pp. 537-544.