Robust state estimation and its application to spacecraft control

Automatica

Volumn 48, Issue 12, 2012, Pages 3142-3150

  Khan, Naeem ^a   Irfan Khattak, M ^a   Gu, Dawei ^b  

^a UNIVERSITY OF ENGINEERING AND TECHNOLOGY   (Pakistan)

^b UNIVERSITY OF LEICESTER   (United Kingdom)

Author keywords

Auto correlation; Kalman filtering; Loss of observation; Open loop estimation; Rigid body spacecraft model; System identification

Indexed keywords

CLOSED-LOOP; ESTIMATION ALGORITHM; ESTIMATION PROBLEM; KALMAN-FILTERING; LINEAR PREDICTION; LINEAR PREDICTION FILTER; MEASURED SIGNALS; MINIMUM MEAN SQUARE ERRORS; OUTPUT DATA; OUTPUT FEEDBACK CONTROLS; PLANT DYNAMICS; REAL-TIME APPLICATION; RIGID BODY SPACECRAFT; ROBUST STATE ESTIMATION; SPACECRAFT APPLICATION; SPACECRAFT CONTROL; SPACECRAFT SYSTEM;

ALGORITHMS; ATTITUDE CONTROL; IDENTIFICATION (CONTROL SYSTEMS); KALMAN FILTERS; ROBUST CONTROL; SPACECRAFT;

ESTIMATION;

EID: 84869497260     PISSN: 00051098     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.automatica.2012.07.002     Document Type: Conference Paper

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