EP2189754A2

Rfog with reduced polarization mode induced bias error

Abstract

Hollow core fiber RFOG having symmetric M- (or W-) shape, three- (or two-) mirror configurations. These symmetric configurations help to cancel out polarization error induced bias of the RFOG even when light of the unwanted ESOP is present. The RFOG resonator with optical components forming substantially small cross-coupling angles between their polarization axes, and/or with polarizing elements inserted into the resonator, and/or with resonator mirrors having identical reflectivity for light of different polarization states, can effectively reduce the polarization mode induced bias error.

EP2189754A2, drawing sheet 1
Sheet 1 of 36

Term

3.2 yearsto projected expiry

Projected expiry 19 November 2029, counted from filing; an application has no term until it is granted.

  1. Priority
  2. Filed
  3. Published
  4. Today
  5. Projected expiry

10 claims: 3 independent, 7 dependent

  1. 1
    An optical gyro comprising:a ring resonator configured to circulate light beams in counter-propagating directions, the ring resonator comprising an optical fiber coil having first and second ends;first and second optical elements configured to receive two input light beams;and transmit a majority of the two input light beams in counter-propagating directions in the ring resonator, the majority of each input light beams entering one of the first and second ends of the optical fiber coil;and a third optical element configured to direct a majority of the circulating light beams in the counter-propagating directions of the ring resonator via the first and second optical elements;and derive a transmission component of the circulating light beams, the transmission component impinging on a photodetector for each of the counter-propagating beams.
  2. 2
    The optical gyro according to Claim 1, wherein the first, second and third optical elements comprise optical mirrors having substantially same reflectivities for light with different polarization states and wherein the optical fiber coil comprises a hollow core fiber.
  3. 3
    The optical gyro according to Claim 1, wherein incidence angles of light beams on the first, second and third optical elements are substantially small for obtaining same reflectivity for light with different polarization states.
  4. 4
    The optical gyro according to Claim 1, further comprising at least one polarizing element with substantially high polarization extinction ratio (PER) located between the first end of the optical fiber coil, and between the second optical element and the second end of the optical fiber coil.
  5. 5
    The optical gyro according to Claim 1, further comprising a housing configured to support the first, second, and third optical elements, the housing having a configuration substantially symmetric dimensions based on Jones matrix.
  6. 6
    An optical gyro comprising:a ring resonator configured to circulate light beams in counter-propagating directions, the ring resonator comprising an optical fiber coil having first and second ends;a first optical element configured to receive two input light beams;and transmit a majority of the two input light beams in counter-propagating directions in the ring resonator, the majority of the input light beams entering one of the first and second ends of the optical fiber coil;and a second optical element configured to direct a majority of the circulating light beams in the counter-propagating directions of the ring resonator via the first and second optical elements;and derive a transmission component of the circulating light beams, the transmission component impinging on a photodetector for each of the counter-propagating beams.
  7. 7
    The optical gyro according to Claim 6, wherein the first and second optical elements comprise optical mirrors having substantially same reflectivities for light with different polarization states.
  8. 8
    The optical gyro according to Claim 6, wherein incidence angles of light beams on the first and second optical elements are substantially small to obtain same reflectivity for light with different polarization states.
  9. 9
    The optical gyro according to Claim 6, wherein angles among at least one of a primary polarizing axis or planes of incidence of all the optical elements are substantially small, the optical gyro further comprising a housing configured to support the first, second, and third optical elements, the housing having a configuration substantially symmetric based on Jones matrix.
  10. 10
    A method comprising:receiving two input light beams at at least one first optical element;transmitting a majority of the two input light beams in counter-propagating directions in a ring resonator having optical fiber coil having first and second ends, the majority of the input light beams entering one of the first and second ends of the optical fiber coil;receiving the counter-propagating light beams from the first and second ends of the optical fiber coil;directing the received counter-propagating light beams to a second optical element;at the second optical element directing a majority of the directed counter-propagating light beams to the optical fiber coil via the at least one first optical element;and directing a portion of the directed counter-propagating light beams to at least one photodetector.