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Research study on stabilization and control: Modern sampled-data control theory. Continuous and discrete describing function analysis of the LST systemThe dynamics of the Large Space Telescope (LST) control system were studied in order to arrive at a simplified model for computer simulation without loss of accuracy. The frictional nonlinearity of the Control Moment Gyroscope (CMG) Control Loop was analyzed in a model to obtain data for the following: (1) a continuous describing function for the gimbal friction nonlinearity; (2) a describing function of the CMG nonlinearity using an analytical torque equation; and (3) the discrete describing function and function plots for CMG functional linearity. Preliminary computer simulations are shown for the simplified LST system, first without, and then with analytical torque expressions. Transfer functions of the sampled-data LST system are also described. A final computer simulation is presented which uses elements of the simplified sampled-data LST system with analytical CMG frictional torque expressions.
Document ID
19740022189
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
January 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-120331
Report Number: NASA-CR-120331
Accession Number
74N30302
Funding Number(s)
CONTRACT_GRANT: NAS8-29853
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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