Attitude Determination GPS/INS Integration System Design Using Triple Difference Technique

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چکیده

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Attitude Determination GPS/INS Integration System Design Using Triple Difference Technique

GPS attitude outputs or carrier phase observables can be effectively utilized to compensate the attitude error of the strapdown inertial navigation system. However, when the integer ambiguity is not correctly resolved and/or a cycle slip occurs, an erroneous GPS output can be obtained. If the erroneous GPS output is applied to the attitude determination GPS/INS (ADGPS/INS) integrated navigation...

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ژورنال

عنوان ژورنال: Journal of Electrical Engineering and Technology

سال: 2012

ISSN: 1975-0102

DOI: 10.5370/jeet.2012.7.4.615