Patent · US Active

Systems and method for gyroscope calibration

US8915116B2 · kind B2 · utility

3Cited by
13References
15Claims
0Family size

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Key dates

Filing dateJan 23, 2013
Grant dateDec 23, 2014
Priority date
Expiry dateJun 21, 2033

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01C25/005
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A mechanism by which a MEMS gyroscope sensor can be calibrated using data gathered from other sensors in a system incorporating the MEMS gyroscope sensor is provided. Data gathered from an accelerometer and a magnetometer in fixed orientation relative to the gyroscope is used to calculate changes in orientation of a system. A constant acceleration vector measured by the accelerometer and a constant magnetic vector measured by the magnetometer are used as reference vectors in a solution to Wahba's problem to calculate a rotation matrix providing the system's orientation with respect to those two constant vectors. By comparing changes in orientation from one time to a next time, measured rates of angular change can be calculated. The measured rates of angular change can be used along with observed gyroscope rates of angular change as input to a linear regression algorithm, which can be used to compute gyroscope trim parameters.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.