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Research study on stabilization and control. Modern sampled-data control theory: Stability analysis of the low cost large space telescope systemThe pointing stability of the low-cost large space telescope (LST) system was investigated. The low-cost LST is characterized by the use of reaction wheels for the generation of control torques. Because of the critical requirement on the pointing accuracy of the LST, the nonlinear frictional characteristics of the bearings of the reaction wheels were studied which can cause limit cycles in a closed-loop system. Another possible source of pointing error in the LST is due to the effect of quantization and sensor noise. Since the LST is a digital system, digital to analog and analog to digital converters and sensors for positional and rate feedbacks were used. Sensor noise and amplitude quantization causes pointing error in the LST and, in addition, quantization is a nonlinear phenomenon which can cause self-sustained oscillations in the closed-loop system. The dynamic modeling of the single-axis LST is described, and several methods of evaluating the attitude error of the digital LST due to quantization and noise inputs are given.
Document ID
19750022882
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kuo, B. C.
(Systems Research Labs., Inc. Champaign, IL, United States)
Singh, G.
(Systems Research Labs., Inc. Champaign, IL, United States)
Date Acquired
September 3, 2013
Publication Date
June 30, 1975
Subject Category
Astronomy
Report/Patent Number
NASA-CR-143933
Report Number: NASA-CR-143933
Accession Number
75N30955
Funding Number(s)
CONTRACT_GRANT: NAS8-29853
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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