Accuracy improvement of SINS based on IMU rotational motion

IEEE Aerospace and Electronic Systems Magazine

Volumn 27, Issue 8, 2012, Pages 4-10

  Sun, Wei ^a   Xu, Ai Gong ^a   Che, Li Na ^a   Gao, Yang ^b  

^a LIAONING TECHNICAL UNIVERSITY   (China)

^b UNIVERSITY OF CALGARY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ACCURACY IMPROVEMENT; BOEING COMPANIES; CERTAIN RULE; COMPUTER TECHNOLOGY; DUAL AXIS; ERROR REDUCTION; GUIDED MISSILES; HIGH PRECISION; HISTORICAL DEVELOPMENT; IMPROPER-ROTATION; INERTIAL SENSOR; INTEGRATED NAVIGATION; INTERNAL SENSORS; MOBILE OBJECTS; MULTI-AXIS; NAVIGATION ACCURACY; NAVIGATION DEVICES; NAVIGATION ERROR; OPERATING PRINCIPLES; POSITION ACCURACY; POSITION ERRORS; ROTATION ANGLES; ROTATION AXIS; ROTATION PLATFORM; ROTATIONAL AXES; ROTATIONAL MOTION; SINGLE-AXIS; THREE-AXIS;

ERRORS; EXPERIMENTS; GYROSCOPES; INDUSTRY; MACHINERY; NAVIGATION; ROTATION; ROTATIONAL FLOW; SUBMARINES; WARSHIPS;

INERTIAL NAVIGATION SYSTEMS;

EID: 84867525094     PISSN: 08858985     EISSN: None     Source Type: Journal    
DOI: 10.1109/MAES.2012.6329155     Document Type: Article

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