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D. T. M. Davis, Jr. coauthored the 1963 paper Rotation Rate Sensing with Traveling-wave Ring Lasers by W. M. Macek and D. T. M. Davis, Jr. with W. M. Macek. Its byline places both at Sperry Gyroscope Company. They reported rotation sensing with a continuously operating helium-neon laser in a square optical cavity, with counterpropagating beams combined at a detector.^[ref]

The measurement reads beating between optical fields. For two fields of frequencies $f_1,f_2$, a simple equal-amplitude model gives a detector term proportional toThe detector can therefore register the difference frequency without resolving either optical oscillation separately. In a ring laser gyroscope, the Sagnac effect makes that difference depend on angular velocity. This mathematical readout model explains why combining the two outputs matters; a pair of beam-power readings alone does not supply their frequency difference. The initial-only name above retains the verified publication identity.

A ring laser gyroscope measures a component of angular velocity from the frequency difference between two counter-circulating waves of a ring laser. Rotation changes their round-trip propagation times through the Sagnac effect. The active optical cavity converts this propagation difference into different resonant frequencies; combining the output waves gives an electrical beat signal through optical heterodyne detection.

For a planar evacuated ideal ring, let $P$ be its full perimeter, $\mathbf{A}$ its oriented vector area, $\mathbf{\Omega }$ its angular velocity and $\lambda$ the nominal vacuum wavelength. At small rotation speed the round-trip time difference has magnitude $|\Delta T|\simeq 4|\mathbf{A}\cdot \mathbf{\Omega }|/c^2$. With $T_0=P/c$ and nominal optical frequency ${\nu }_0=c/\lambda$, the resonant-frequency difference has magnitude ${\nu }_0|\Delta T|/T_0$. Choosing the output sign consistently with the area orientation givesThis is an ideal first-order scale law, with reciprocal paths and resolved counter-circulating modes. Optical dispersion and actual apparatus behaviour require a fuller response model. The underlying circulation-time difference is the one measured by a Sagnac interferometer.^[ref]

For an original square ring with $0.10\mathrm{m}$ sides, $A=0.010{\mathrm{m}}^2$ and $P=0.40\mathrm{m}$. At $\lambda =632.8\mathrm{nm}$ and normal-axis rotation $\Omega =0.010rad/s$,Tilting the ring changes the measured projection, not the full rotation magnitude. Reconstructing a general rotation vector requires independent directional information. The kilohertz-scale difference is also distinct from the optical carrier frequency and the cavity's free spectral range.

A historical experiment made the frequency comparison concrete. W. M. Macek and D. T. M. Davis, Jr. reported rotation sensing in 1963 using a continuous-wave helium-neon ring laser on the $1.153\mu \mathrm{m}$ line. Their metre-square apparatus used four gas tubes with Brewster windows and four external corner mirrors. The first-page diagram directs the two beams toward combining optics and a photocathode, linking the geometric circulation difference to a detectable beat.^[ref]

For two coherent output powers $I_1,I_2$, the ideal combined signal includesOne such intensity record supplies a beat-frequency magnitude, not automatically the rotation sign, since changing the sign can be absorbed into the unknown phase. A directional readout needs additional phase information or a suitable reference. Mode coupling, frequency bias and detector response must also be tested rather than treating a closed optical path as a complete calibrated sensor.

W. M. Macek coauthored Rotation Rate Sensing with Traveling-wave Ring Lasers by W. M. Macek and D. T. M. Davis, Jr. with D. T. M. Davis, Jr. in 1963. Their Sperry Gyroscope Company experiment used the $1.153\mu \mathrm{m}$ line of a helium-neon laser in a metre-square optical cavity. Four gas tubes and four corner mirrors maintained the ring path, and the outputs were combined for detection.^[ref]

Their contribution illustrates the distinction between a passive Sagnac interferometer and an active ring laser gyroscope: the circulating optical fields are sustained by laser gain, and their frequency splitting provides a rotation signal. In the ideal planar model, the magnitude of the split iswhere $A$ is the enclosed area, $P$ the ring perimeter, $\lambda$ the wavelength and ${\Omega }_n$ the component of angular velocity normal to the ring. This follows by converting the Sagnac effect's counterpropagating travel-time difference into a resonant frequency difference.

For an original ideal scale calculation using the reported square size and wavelength, take $A=1{\mathrm{m}}^2$, $P=4\mathrm{m}$ and $|{\Omega }_n|=10^{-4}rad/s$. Then $|\Delta f|\approx 86.73\mathrm{Hz}$. Doubling the side of a square doubles $A/P$ and this scale factor. These are model calculations, not reported sensitivity or accuracy figures. The joint paper establishes the demonstrated apparatus, without assigning its component tasks to either author separately.