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High accuracy precession measurement with an autometric gyro
Authors:David I Shalloway  David H Frisch
Institution:(1) Department of Physics and Center for Space Research, Massachusetts Institute of Technology, Cambridge, Massachusetts, USA
Abstract:A simple reticle with parallel equally spaced lines to transmit light in an autometric gyro is shown to give a signal which can be used for very accurate angular precession measurements. Frequency analysis of the signal is chosen over time domain analysis and/or over a specially designed reticle.Gyro precession will induce a change in the interference structure of the spectrum in addition to dilating the overall frequency distribution. The expected output spectrum has been analytically determined, exhibiting the dependence on spot and reticle line cross sections and line spacing so that they can be precisely determined from the output data.The spectrum structure is extremely sensitive to precession. Computer simulations indicate that accuracy will be limited by reticle line spacing variations to ±4×10–9 rad. This would allow a Lense-Thirring precession measurement accurate to ±20% in 30 days (accuracy being limited by physical effects common to all such experiments) or a ±1% de Sitter precession measurement in four days.Nomenclature a n(rhov) Fourier coefficients ofI(theta) - a n r (rhov) rapidly varying part ofa n(rhov) - a m x ,b m x Fourier coefficients ofI(x) - a psgr(rhov),b psgr(rhov) Fourier sine and cosine transforms ofpsgr x(x) - agr angle between star and gyro spin axis - agr0 initial alignment angle - f focal length of optical system - I transmitted light intensity, signal function - l reticle line width - r distance from light spot center - R light-circle radius - rhov= 
$$\frac{{2\pi R}}{{l + s}}$$
reduced light-circle radius - rhov 0 reduced reticle center-spin center offset - s reticle line space - T(x) reticle transmission function - theta angle of gyro rotation - w g gyro angular velocity This work was supported by the M.I.T. Center for Space Research under NASA Grant NGL-22-009-019.
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