Inner Attitude Integration Algorithm Based on Fault Detection for Strapdown Inertial Attitude and Heading Reference System

Chinese Journal of Aeronautics

Volumn 23, Issue 1, 2010, Pages 68-74

  Jianye, Liu ^a   Yanhua, Zhu ^a   Jizhou, Lai ^a   Yongjun, Yu ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

inner attitude integration algorithm; internal damping; Kalman filter; navigation; residual chi square test; strapdown inertial attitude and heading reference system

Indexed keywords

ATTITUDE ACCURACY; ATTITUDE ERROR; ATTITUDE MEASUREMENT; CHI-SQUARE TESTS; INERTIAL MEASURING UNIT; INTEGRATION ALGORITHM; INTERNAL DAMPING; REAL SYSTEMS; REAL TIME; REFERENCE SYSTEMS; STATIC STATE;

ACCELEROMETERS; ALGORITHMS; FAULT DETECTION; INERTIAL NAVIGATION SYSTEMS; KALMAN FILTERS; NAVIGATION;

DAMPING;

EID: 77950303822     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(09)60189-8     Document Type: Article

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