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Published in 2022 at "IEEE Access"
DOI: 10.1109/access.2022.3180364
Abstract: For the Inertial Navigation System (INS) in hypersonic flight, when the centroid of the Inertial Measurement Unit (IMU) does not coincide with that of hypersonic vehicle, a lever-arm effect error will be generated, which will…
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Keywords:
arm effect;
arm;
dynamic lever;
error ... See more keywords