Autonomous failure detection, identification and fault-tolerant estimation with aerospace applications

IEEE Aerospace Conference Proceedings

Volumn 2, Issue , 1998, Pages 133-138

  Mehra, R ^a   Rago, C ^a   Seereeram, S ^a  

^a Scientific Systems Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; NONLINEAR SYSTEMS; STAR TRACKERS; AEROSPACE ENGINEERING; COMPUTER SIMULATION; KALMAN FILTERING; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION;

ACTUATOR FAILURES; DETECTION AND IDENTIFICATIONS; FAILURE DETECTION; HIGH-FIDELITY SIMULATIONS; INTERACTING MULTIPLE MODEL; MULTI-HYPOTHESIS; SPACECRAFT AUTONOMY; VALIDATION TESTING;

EXTENDED KALMAN FILTERS; FAULT TOLERANT COMPUTER SYSTEMS;

EXTENDED KALMAN FILTER (EKF) METHOD; INTERACTING MULTIPLE MODELS (IMM);

EID: 0031631294     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.1998.687904     Document Type: Conference Paper

References (9)

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8. Mehra, R.K., and S. Seereeram (1994) "Neural Nets and Adaptive Reconfigurable Spacecraft Guidance and Control under Failure Conditions," Technical Report 931-09.03-5355, Scientific Systems Company Inc., July 1994.
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