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Optical Engineering

Observational model for microarcsecond astrometry with the Space Interferometry Mission
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Paper Abstract

The Space Interferometry Mission (SIM) is a space-based long-baseline optical interferometer for precision astrometry. One of the primary objectives of the SIM instrument is to accurately determine the directions to a grid of stars, together with their proper motions and parallaxes, improving a priori knowledge by nearly three orders of magnitude. The basic astrometric observable of the instrument is the path-length delay, a measurement made by a combination of internal metrology measurements that determine the distance the starlight travels through the two arms of the interferometer and a measurement of the white light stellar fringe to find the point of equal path length. Because this operation requires a nonnegligible integration time to accurately measure the stellar fringe position, the interferometer baseline vector is not stationary over this time period, as its absolute length and orientation are time-varying. This conflicts with the consistency condition necessary for extracting the astrometric parameters, which requires a stationary baseline vector. We address how the time-varying baseline is "regularized" so that it can act as a single baseline vector for multiple stars, and thereby establishing the fundamental operation of the instrument.

Paper Details

Date Published: 1 July 2003
PDF: 11 pages
Opt. Eng. 42(7) doi: 10.1117/1.1576405
Published in: Optical Engineering Volume 42, Issue 7
Show Author Affiliations
Mark H. Milman, Jet Propulsion Lab. (United States)
Slava G. Turyshev, Jet Propulsion Lab. (United States)


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