Method for measuring force-dependent gyroscope sensitivity

Data processing: measuring – calibrating – or testing – Calibration or correction system – Direction

Reexamination Certificate

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C702S041000, C073S504020, C073S504080, C073S504180

Reexamination Certificate

active

06904377

ABSTRACT:
System and method for measuring force-dependent gyroscopic sensitivity. A force-effect model of the effects of acceleration on the output of a gyro triad is determined. Rotation sequences are then devised to permit excitation and observation of force-effect model parameters in order to provide calibration information for these parameters. A state diagram containing the gyro triad force-effect model parameters is derived from the force-effect model, where moving from one position in the state diagram to another position indicates the gyro triad error which would occur in rotating the gyro triad according to a corresponding motion. Searching for all possible closed loop paths achievable through the state diagram, by a multiple-axes rate table with a specified number of rotations, to separate gyro triad error calibration from the accelerometer calibration. Closed loop paths having minimal lengths and exhibiting larger error sensitivity are chosen to perform error parameter calibration and reduce force-dependent gyroscopic sensitivity.

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patent: 5570304 (1996-10-01), Mark et al.
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patent: 2003/0084704 (2003-05-01), Hanse
patent: 1 059 509 (2000-09-01), None
patent: WO 00/48883 (2000-08-01), None
“Fast Orthogonal Calibration of a Ring Laser Strapdown System,” by John Mark, Daniel Tazartes, Timothy Hilby, Symposium Gyro Technology, Sep. 1986, Stuttgart, West Germany.

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