Application of quaternion-based extended Kalman filter for MAV attitude estimation using MEMS sensors

Nami Jishu yu Jingmi Gongcheng/Nanotechnology and Precision Engineering

Volumn 7, Issue 2, 2009, Pages 163-167

  Xue, Liang ^a   Yuan, Wei Zheng ^a   Chang, Hong Long ^a   Qin, Wei ^a   Yuan, Guang Min ^a   Jiang, Cheng Yu ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Attitude estimation; Extended Kalman filter; Gauss Newton; MEMS gyroscope; Quaternion

Indexed keywords

ATTITUDE ESTIMATION; ESTIMATED ERRORS; EXTENDED KALMAN FILTER ALGORITHMS; GAUSS-NEWTON; GAUSS-NEWTON ALGORITHMS; MANEUVERING ACCELERATIONS; MEMS GYROSCOPE; MEMS SENSORS; MICRO AERIAL VEHICLES; QUATERNION; STATE EQUATIONS; STATE VECTORS; STOCHASTIC ERROR MODELS; WELL TRACKS;

CELLULAR RADIO SYSTEMS; CONTROL THEORY; ERRORS; ESTIMATION; EXTENDED KALMAN FILTERS; MANEUVERABILITY; MEMS; MICROELECTROMECHANICAL DEVICES; MICROSENSORS; POSITION CONTROL; STOCHASTIC MODELS;

GYROSCOPES;

EID: 64849114547     PISSN: 16726030     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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