Patent · US Active

Inertial sensor fusion orientation correction

US9068843B1 · kind B1 · utility

22Cited by
4References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 26, 2014
Grant dateJun 30, 2015
Priority date
Expiry dateSep 26, 2034

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH04W4/027
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

A system for determining and correcting a calculated orientation of a computing device based on data from an accelerometer and a gyroscope. The system compares a predicted direction of gravity in a predicted frame of the device with a measured direction of gravity in a sensor frame of the device, and determines an angle of the difference between the directions. A correction is calculated to rotate the predicted frame around an axis by the angle relative to a sensor frame, the axis being perpendicular to both the predicted and measured directions of gravity. A predicted orientation of a reference “Earth” frame relative to the predicted frame is calculated based on the gyroscope data. A corrected orientation is determined by applying the correction to the predicted orientation, providing an orientation of the Earth reference frame relative to the sensor frame.

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