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The 15-meter antenna performance optimization using an interdisciplinary approach

Authors :
Grantham, William L
Schroeder, Lyle C
Bailey, Marion C
Campbell, Thomas G
Source :
Jet Propulsion Lab., Proceedings of the Mobile Satellite Conference.
Publication Year :
1988
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1988.

Abstract

A 15-meter diameter deployable antenna has been built and is being used as an experimental test system with which to develop interdisciplinary controls, structures, and electromagnetics technology for large space antennas. The program objective is to study interdisciplinary issues important in optimizing large space antenna performance for a variety of potential users. The 15-meter antenna utilizes a hoop column structural concept with a gold-plated molybdenum mesh reflector. One feature of the design is the use of adjustable control cables to improve the paraboloid reflector shape. Manual adjustment of the cords after initial deployment improved surface smoothness relative to the build accuracy from 0.140 in. RMS to 0.070 in. Preliminary structural dynamics tests and near-field electromagnetic tests were made. The antenna is now being modified for further testing. Modifications include addition of a precise motorized control cord adjustment system to make the reflector surface smoother and an adaptive feed for electronic compensation of reflector surface distortions. Although the previous test results show good agreement between calculated and measured values, additional work is needed to study modelling limits for each discipline, evaluate the potential of adaptive feed compensation, and study closed-loop control performance in a dynamic environment.

Subjects

Subjects :
Communications And Radar

Details

Language :
English
Database :
NASA Technical Reports
Journal :
Jet Propulsion Lab., Proceedings of the Mobile Satellite Conference
Publication Type :
Report
Accession number :
edsnas.19880016362
Document Type :
Report