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Elevation control system model for the DSS 13 antennaIn order to meet the requirements for precision pointing of 34-m antennas, adequate control design and simulation software have to be developed along with a detailed description of the supporting analytical tools. This article describes a control system model for the elevation drive of the DSS 13 antenna. The model allows one to simulate elevation dynamics, cross-coupled dynamics in azimuth and elevation, and RF pointing error. A modal state-space model of the antenna structure was obtained from its finite-element model with a free rotating tipping structure. Model reduction techniques were applied separately for the antenna model and rate-loop model, thereby reducing the system order to one-third of the original one while preserving its dynamic properties. Extensive simulation results illustrate properties of the model.
Document ID
19940025119
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gawronski, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mellstrom, J. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 15, 1991
Publication Information
Publication: The Telecommunications and Data Acquisition Report
Subject Category
Mechanical Engineering
Accession Number
94N29622
Funding Number(s)
PROJECT: RTOP 314-40-42-10-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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