Applying the principle of integrated navigation systems to estimating the motion of large vehicles

Aerospace Science and Technology

Volumn 8, Issue 2, 2004, Pages 155-166

  Wagner, Jörg F ^a   Kasties, G ünther ^b  

^a UNIVERSITY OF STUTTGART   (Germany)

^b Oecon GmbH   (Germany)

Author keywords

Flexible structure; Inertial sensor; Integrated navigation system; Kalman filter; Satellite navigation

Indexed keywords

ACCELEROMETERS; AEROSPACE VEHICLES; DATA PROCESSING; DEGREES OF FREEDOM (MECHANICS); FLEXIBLE STRUCTURES; KALMAN FILTERING; MATHEMATICAL MODELS; SENSORS; SPACE STATIONS; VECTORS;

INERTIAL SENSORS; INTEGRATED NAVIGATION SYSTEM; SATELLITE NAVIGATION;

NAVIGATION;

EID: 1242320308     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2003.09.006     Document Type: Article

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