Optimization-based alignment for inertial navigation systems: Theory and algorithm

Aerospace Science and Technology

Volumn 15, Issue 1, 2011, Pages 1-17

  Wu, Meiping ^a   Wu, Yuanxin ^a   Hu, Xiaoping ^a   Hu, Dewen ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

Alignment; Eigenvector; Global observability; Inertial navigation system

Indexed keywords

ALIGNMENT METHODS; ANGULAR MOTIONS; ATTITUDE DETERMINATION; EIGENVECTORS; ERROR EQUATION; EULER ANGLES; EXPERIMENT TESTS; FILTERING TECHNIQUE; GLOBAL OBSERVABILITY; GYROCOMPASSING; HIGH FREQUENCY HF; INERTIAL NAVIGATIONS; OPTIMIZATION METHOD; OPTIMIZATION PROBLEMS; SENSOR BIAS; SIMULATION STUDIES; TRANSLATIONAL MOTIONS; VECTOR OBSERVATIONS;

EIGENVALUES AND EIGENFUNCTIONS; INERTIAL NAVIGATION SYSTEMS; NAVIGATION; OBSERVABILITY; OPTIMIZATION; SENSITIVITY ANALYSIS; SENSORS;

ALIGNMENT;

EID: 78751580530     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2010.05.004     Document Type: Article

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