Fault detection and diagnosis in a spacecraft attitude determination system

Acta Astronautica

Volumn 65, Issue 5-6, 2009, Pages 710-729

  Pirmoradi, F N ^a   Sassani, F ^a   de Silva, C W ^a  

^a UNIVERSITY OF BRITISH COLUMBIA   (Canada)

Author keywords

Attitude determination; Diagnosis; Fault detection; Health monitoring; Kalman filter; Spacecraft

Indexed keywords

ANGULAR POSITIONS; ATTITUDE DETERMINATION; ATTITUDE DETERMINATION SYSTEMS; ATTITUDE ESTIMATION; FAULT DETECTION AND DIAGNOSIS; FAULT ISOLATION; FAULT SIGNATURE; GENERALIZED LIKELIHOOD RATIO TEST; GYRO BIAS; HEALTH MONITORING; INNOVATION SEQUENCE; LINEARIZED KALMAN FILTERS; MEASUREMENT DATA; MODEL-BASED; MULTIPLE HYPOTHESIS; RATE GYRO; ROTATIONAL DYNAMICS; SECOND PHASE; SENSOR MEASUREMENTS; SENSOR OUTPUT; SPACECRAFT ATTITUDE DETERMINATION; STATE ESTIMATES; SYSTEM KINEMATICS; TWO PHASIS; VECTOR SENSORS;

CELLULAR RADIO SYSTEMS; CONTROL THEORY; ESTIMATION; EXTENDED KALMAN FILTERS; GYROSCOPES; KINEMATICS; MAXIMUM LIKELIHOOD ESTIMATION; MEASUREMENT ERRORS; MONITORING; ORTHOGONAL FREQUENCY DIVISION MULTIPLEXING; SENSORS; SPACECRAFT; SPEECH RECOGNITION; STATE ESTIMATION; STATISTICAL TESTS; STRUCTURES (BUILT OBJECTS);

FAULT DETECTION;

EID: 67349184838     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2009.03.002     Document Type: Article

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