Method of reducing polarization fluctuation inducing drift in resonator fiber optic gyro
AssigneeTokyo Aircraft Instrument Co., Ltd.
InventorsSuminori Honda, Kazuo Hotate
Life of this patent
Estimating the term…
Loading patent…
AssigneeTokyo Aircraft Instrument Co., Ltd.
InventorsSuminori Honda, Kazuo Hotate
Estimating the term…
There is provided a method of generating no error in the output of a resonator fiber optic gyro even when the polarization dependency loss is present in a ring resonator of the resonator fiber optic gyro. The relationship between ΔL and Δβ is set to satisfy the formula ΔβΔL=π+2nπ [radian] (n: integer), or ΔβΔL is close to the value obtained from the formula, where ΔL is defined as the difference between the lengths L1 and L2 of two portions of a waveguide divided by a coupler and a polarization-rotating point in the ring resonator, and Δβ is defined as the difference in propagation constant of two axes of polarization having the waveguide. ΔL is set so that the error induced by the polarization fluctuation is minimized. Even when the polarization dependency loss is present in the coupler or the like, the ring resonator itself generates no errors thereby, and the error of the gyro output induced by the polarization fluctuation can be minimized in the resonator fiber optic gyro.
A method of reducing the polarization fluctuation inducing drift in a resonator fiber optic gyro, comprising the step of:
A method of reducing the polarization fluctuation inducing drift in a resonator fiber optic gyro, comprising the step of:
A method of reducing the polarization fluctuation inducing drift in a resonator fiber optic gyro, comprising the step of:
Dependencies are inferred from the claim text.