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Large space system control technology status and accomplishmentsIn the area of antenna modeling and control, preliminary structural models were defined for two representative parabolic reflectors. A control system design evolved for attitude control of the reflectors. The controller design was based on a lumped control concept where the control hardware (sensor and actuators) was mounted at the base of the antenna. In the area of distributed control, static shape control techniques were worked out to establish a prescribed vehicle shape. The corresponding estimation process for determination of vehicle shape from selected sensor measurements was also developed. A model order reduction study was conducted to find the best preflight dynamical models for on board controller design. The problems caused by truncation of the vehicle dynamics required to minimize on board computations were investigated. Estimator designs were developed for on board detection of large structure model errors.
Document ID
19800010886
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rodriguez, G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Parker, G. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
February 1, 1980
Publication Information
Publication: NASA. Langley Res. Center Large Space Systems Technol., 1979
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
80N19163
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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