Patent · US Active

Integrated photonics optical gyroscopes optimized for autonomous terrestrial and aerial vehicles

US11656081B2 · kind B2 · utility

1Cited by
40References
22Claims
0Family size

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Key dates

Filing dateOct 15, 2020
Grant dateMay 23, 2023
Priority date
Expiry dateOct 15, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG02B2006/12138
  • WIPO fieldOptics
  • WIPO sectorInstruments

Abstract

Novel small-footprint integrated photonics optical gyroscopes disclosed herein can provide ARW in the range of 0.05°/√Hr or below (e.g. as low as 0.02°/√Hr), which makes them comparable to fiber optic gyroscopes (FOGs) in terms of performance, at a much lower cost. The low bias stability value in the integrated photonics optical gyroscope corresponds to a low bias estimation error (in the range of 1.5°/Hr or even lower) that is crucial for safety-critical applications, such as calculating heading for autonomous vehicles, drones, aircrafts etc. The integrated photonics optical gyroscopes may be co-packaged with mechanical gyroscopes into a hybrid inertial measurement unit (IMU) to provide high-precision angular measurement for one or more axes.

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