Tightly-coupled INS/GPS using quaternion-based unscented Kalman filter

AIAA Guidance, Navigation, and Control Conference 2011

Volumn , Issue , 2011, Pages

  Zhou, Junchuan ^a   Yang, Yuhong ^a   Zhang, Jieying ^a   Edwan, Ezzaldeen ^a   Loffeld, Otmar ^a   Knedlik, Stefan ^b  

^a UNIVERSITY OF SIEGEN   (Germany)

^b IMAR GmbH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; GLOBAL POSITIONING SYSTEM; INERTIAL NAVIGATION SYSTEMS;

ACCURATE ESTIMATION; FIELD EXPERIMENT; INERTIAL SENSOR; INS/GPS INTEGRATION; NUMERICAL RESULTS; OBSERVATION MODEL; SINGULARITY PROBLEMS; UNSCENTED KALMAN FILTER;

KALMAN FILTERS;

EID: 85086492198     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2011-6488     Document Type: Conference Paper

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