Apparatus and method for the elimination of angular vibration induced errors in ring laser gyroscopes

Claim 2

In a sinusoidally dithered ring laser gyroscope wherein clockwise and counterclockwise light beams are generated in the optical cavity of the gyroscope and wherein the frequency differential between the two beams caused by rotation of the gyroscope results in an interference pattern when the beams are extracted from the gyroscope and heterodyned by a beam combining means and wherein the beat frequency of the interference pattern is measured by a photodetector and wherein the beat frequency is a measure of the angular rotation of the gyroscope and wherein means including the photodetector convert the measure of beat frequency to a gyroscope output signal indicating the angular rotation of the gyroscope, an apparatus comprising: (a) said photodetector including at least one analog gyroscope output signal in the form V(t) =Vp sin (Ψ+β+φ) where Vp is a scale factor related to the excitation voltage of the photodetector means, Ψ is the momentary phase difference between the clockwise and counterclockwise beams, β is the composite scattering angle and φ is the fringe pattern adjustment for any phase which can be adjusted by positioning of the photodetector means; (b) the excitation voltage of the photodetector being scaled such that ##EQU5## where Ω L is the rate at which lock-in effect occurs in the gyroscope Ω D is the dither rate of the gyroscope and ω d is the dither frequency of the gyroscope; (c) the fringe pattern adjustment φ being set at -π/4; (d) means to sense said analog gyroscope output signal when the dither velocity is zero to obtain an error signal proportional to the phase error due to the lock-in phenomenon at said time; and (e) means to add said error signal to the gyroscope output signal to correct for phase errors due to the lock-in phenomenon.

Claim 3

The apparatus of claim 1 wherein said gyroscope includes means to digitize said analog gyroscope output signal forming upcounts and downcounts for use in generating a digital gyroscope output signal and in which said means to add is comprised of: (a) an analog to digital converter which transforms the amplitude of said analog output signal from the photodetector into digital form; (b) an accumulator which compiles the digital signal from the analog to digital converter at every point of zero dither velocity and generates an overflow or borrow pulse when the compiled signal reaches 2π; and (c) means for adding the overflow and borrow pulses to the output of said means to digitize.

Claim 4

The apparatus of claim 2 wherein said means for adding the overflow or borrow pulse to the outpt of said means to digitize comprise an OR gate.

Claim 5

In a sinusoidally dithered ring laser gyroscope wherein clockwise and counterclockwise light beams are generated in the optical cavity of the gyroscope and wherein the frequency differential between the two beams caused by rotation of the gyroscope results in an interference pattern when the beams are extracted from the gyroscope and heterodyned by a beam combining means and wherein the beat frequency of the interference pattern is measured by a photodetector and wherein the beat frequency is a measure of the angular rotation fo the gyroscope and wherein means including the photodetector convert the measure of beat frequency to a gyroscope output signal indicating the angular rotation of the gyroscope, a method of eliminating errors due to lock-in effects, which comprises: (a) generating at least one analog gyroscope output signal in the form V(t)=Vp sin (Ψ+β+φ) where Vp is a scale factor related to the excitation voltage of the photodetector means, Ψ is the momentary phase difference between the clockwise and counterclockwise beams, β is the composite scattering angle and φ is the fringe pattern adjustment for any phase which can be adjusted by positioning of the photodetector means; (b) scaling the excitation voltage of the photodetector so that ##EQU6## where Ω L is the rate at which lock-in effect occurs in the gyroscope, Ω D is the dither rate of the gyroscope and ω d is the dither frequency of the gyroscope; (c) positioning the photodetector so that the fringe pattern adjustment φ is equal to -π/4; (d) sensing said analog gyroscope output signal when the dither velocity is zero to obtain an error signal proportional to the phase error due to the lock-in phenomenon at said time; (e) adding said error signal to the gyroscope output signal to correct for phase errors due to the lock-in phenomenon.

Claim 6

In a sinusoidally dithered ring laser gyroscope wherein clockwise and counterclockwise light beams are generated in the optical cavity of the gyroscope and wherein the frequency differential between the two beams caused by rotation of the gyroscope results in an interference pattern when the beams are extracted from the gyroscope and heterodyned by a beam combining means and wherein the beat frequency of the interference pattern is measured by a photodetector and wherein the beat frequency is a measure of the angular rotation fo the gyroscope and wherein means including the photodetector convert the measure of beat frequency to a gyroscope output signal indicating the angular rotation of the gyroscope, a method of eliminating errors due to lock-in effects, which comprises: (a) generating at least one analog gyroscope output signal in the form V(t)=Vp sin (Ψ+β+φ) where Vp is a scale factor related to the excitation voltage of the photodetector means, Ψ is the momentary phase difference between the clockwise and counterclockwise beams, β is the composite scattering angle and φ is the fringe pattern adjustment for any phase which can be adjusted by positioning of the photodetector means; (b) scaling the excitation voltage of the photodetector so that ##EQU6## where Ω L is the rate at which lock-in effect occurs in the gyroscope, Ω D is the dither rate of the gyroscope and ω d is the dither frequency of the gyroscope; (c) positioning the photodetector so that the fringe pattern adjustment φ is equal to -π/4; (d) sensing said analog gyroscope output signal when the dither velocity is zero to obtain an error signal proportional to the phase error due to the lock-in phenomenon at said time; (e) adding said error signal to the gyroscope output signal to correct for phase errors due to the lock-in phenomenon.