In-flight calibration and alignment of astroinertial system for attititude determination of a maneuvering land-survey satellite

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We have presented discrete algorithms for a filtering of measurements, in-flight calibration and alignment of astroinertial system for the attitude determination of a maneuvering land-survey satellite.

Satellite, attitude determination, astroinertial system, in-flight calibration

Короткий адрес: https://sciup.org/148204825

IDR: 148204825

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