The 34-meter antennas of the NASA Deep Space Network are "wheel and track" antennas. The latter term refers to a set of wheels at the base of the structure, which roll on a circular steel track supported by a concrete foundation ring. The track is assumed flat; however, its level varies due to manufacturing imperfections, structural loads, non-uniformity of the soil, and temperature variations. It is specified that the deviations of the azimuth-track level shall not exceed /spl plusmn/0.5 mm. During tracking, this amplitude of deviations causes deformations of the antenna structure, resulting in pointing errors of /spl plusmn/2 mdeg, which exceed the required accuracy for 32-GHz (Ka-band) tracking. However, structural deformations caused by the azimuth track unevenness are repeatable; therefore, a look-up table can be created to improve the blind-pointing accuracy. This paper presents the process for creation of the look-up table, describes the instrumentation necessary for determining the pointing errors, and describes the processing of inclinometer data. It derives algorithms for the pointing-error estimation, and for the azimuth-axis tilt using the inclinometer data. It compares the error corrections based on the created look-up table and actual measurements of pointing errors using the conical scanning (conscan) technique. This comparison shows a satisfactory convergence that justifies the implementation of the approach in forthcoming NASA missions.
No takes yet. Share an insight, caveat, or question.
Gawroński et al. (2000) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: