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Pointing and Scanning Control of Optical Instruments using Rotating Unbalanced MassesCorrect pointing direction and scanning motions are essential in the operation of many flight payloads, such as balloon-borne telescopes and space-based X- ray and gamma-ray telescopes. Rotating unbalanced mass (RUM) devices have been recently proposed, implemented and successfully tested to produce a variety of scanning motions. Linear scans, raster scans, and circular scans have been successfully generated on a gimbaled payload using pairs of RUM devices. Theoretical analysis, computer simulations, and experiments have also been used to study the feasibility of using RUM devices to control instrument pointing direction, in addition to generating scanning motion. Dynamic modeling of a gimbaled payload equipped with a pair of RUM devices has been studied, and preliminary testing indicates that the pointing control is indeed feasible. However, there is also great potential for significant performance improvements through more advanced control system analysis, modeling and design. In this paper, modeling and control methods are described to achieve simultaneous scanning and pointing control of a gimbaled payload using rotating unbalance mass (RUM) devices. The model development work builds upon the results of Polites et al. and also some modeling approaches from robotics research. Results of some preliminary experiments are discussed and some nonlinear control methods will be proposed.
Document ID
19970025216
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Bishop, Carlee A.
(Auburn Univ. AL United States)
Hung, John Y.
(Auburn Univ. AL United States)
Polites, Michael E.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Alhorn, Dean C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Subject Category
Mechanical Engineering
Report/Patent Number
AAS-97-065
NASA-TM-112521
NAS 1.15:112521
Report Number: AAS-97-065
Report Number: NASA-TM-112521
Report Number: NAS 1.15:112521
Accession Number
97N24830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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