Kalman filter innovation sequence based fault detection in LEO satellite attitude determination and control system

Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007

Volumn , Issue , 2007, Pages 411-416

  Okatan, A ^a   Hajiyev, Ch ^b   Hajiyeva, U ^a  

^a Golden Horn University   (Turkey)

^b ISTANBUL TECHNICAL UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE INDUSTRY; CELLULAR RADIO SYSTEMS; CONTROL THEORY; EXTENDED KALMAN FILTERS; KALMAN FILTERS; MILITARY DATA PROCESSING; MOTION CONTROL; NAVIGATION; ORBITS; PNEUMATIC CONTROL EQUIPMENT; SATELLITES; STATISTICAL METHODS; STATISTICS; WAVE FILTERS;

AND DETECTION; ATTITUDE DYNAMICS; EXTENDED KALMAN FILTER (ITERATED); FAULT DETECTION ALGORITHM; INNOVATION MATRIX; INNOVATION SEQUENCE; INTERNATIONAL CONFERENCES; LEO SATELLITES; MATHEMATICAL EXPECTATIONS; SENSOR FAULTS; SPACE TECHNOLOGY (ST); SPECTRAL NORMS; STATISTICAL CHARACTERISTICS;

FAULT DETECTION;

EID: 46449110619     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/RAST.2007.4284023     Document Type: Conference Paper

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