A Dynamic Attitude Measurement System Based on LINS

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چکیده

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A Dynamic Attitude Measurement System Based on LINS

A dynamic attitude measurement system (DAMS) is developed based on a laser inertial navigation system (LINS). Three factors of the dynamic attitude measurement error using LINS are analyzed: dynamic error, time synchronization and phase lag. An optimal coning errors compensation algorithm is used to reduce coning errors, and two-axis wobbling verification experiments are presented in the paper....

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ژورنال

عنوان ژورنال: Sensors

سال: 2014

ISSN: 1424-8220

DOI: 10.3390/s140916082