Adaptive kalman filter tuning in integration of low-cost MEMS-INS/GPS

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 3, Issue , 2004, Pages 1787-1797

  Basil, Helen ^a   Ananthasayanam, M R ^b   Puri, S N ^a  

^a Indian Institute of Science ^*

^b INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE GAINS; COVARIANCE PROPOGATION; FILTER PARAMETERS; INERTIAL SENSORS;

ACCELEROMETERS; ALGORITHMS; GLOBAL POSITIONING SYSTEM; GYROSCOPES; INERTIAL NAVIGATION SYSTEMS; MICROELECTROMECHANICAL DEVICES; PARAMETER ESTIMATION; SENSORS; SPURIOUS SIGNAL NOISE; STATISTICAL METHODS;

KALMAN FILTERING;

EID: 19944374133     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Britting, K.R. 'Inertial Navigation Systems Analysis'. John Wiley and Sons Inc (1971).
2. Maybeck, P.S, 'Stochastic model, Estimation and Control'- Vol.2, Academic Press Inc.(1979)
3. Candy, J.V., 'Signal Processing -The model based Approach', McGraw Hill co., New York (1986)
4. Myers, K.A and Tapley, B.D. 'Adaptive Sequential Estimation With Unknown Noise Statistics', IEEE Trans automatic Control, Vol. AC 21, pp 520-525, (1976)
5. Gemson R.M.O and Ananthasayanam M.R., 'Importance of Initial State Covariance Matrix For The Parameters Estimation Using An Adaptive Extended Kalman Filter'. Proc. AIAA Conference on Atmospheric Flight Mechanics AIAA-98-4153. (1998).