Study on innovation adaptive EKF for in-flight alignment of airborne POS

IEEE Transactions on Instrumentation and Measurement

Volumn 60, Issue 4, 2011, Pages 1378-1388

  Jiancheng, Fang ^a   Sheng, Yang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Extended Kalman filter (EKF); In flight alignment (IFA); innovation based adaptive estimation (IAE); Position and Orientation measurement System (POS); real time performance; Strapdown Inertial Navigation System (SINS) Global Positioning System (GPS) integrated navigation system

Indexed keywords

ADAPTIVE ESTIMATION; ADAPTIVE FILTERING ALGORITHMS; AIRBORNE REMOTE SENSING; ALIGNMENT ACCURACY; COMPUTATIONAL BURDEN; FILTER GAIN MATRIX; HEADING ERROR; IN-FLIGHT ALIGNMENT; IN-FLIGHT ALIGNMENT (IFA); INITIAL ALIGNMENT; INTEGRATED SYSTEMS; MATRIX MULTIPLICATION; MEASUREMENT NOISE; ORIENTATION MEASUREMENTS; POSITION AND ORIENTATION MEASUREMENT SYSTEM (POS); REAL-TIME PERFORMANCE; STRAP-DOWN INERTIAL NAVIGATION SYSTEMS; TURNING MANEUVERS;

ADAPTIVE ALGORITHMS; ADAPTIVE FILTERING; ADAPTIVE FILTERS; ALIGNMENT; COVARIANCE MATRIX; ESTIMATION; EXPERIMENTS; EXTENDED KALMAN FILTERS; INERTIAL NAVIGATION SYSTEMS; INTEGRATED OPTICS; INTEGRATION; ION BEAMS; MEASUREMENTS; NAVIGATION; POSITION CONTROL; REMOTE SENSING;

GLOBAL POSITIONING SYSTEM;

EID: 79952577842     PISSN: 00189456     EISSN: None     Source Type: Journal    
DOI: 10.1109/TIM.2010.2084710     Document Type: Article

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