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Dynamics and control simulation of large space structuresAttention is given to the dynamics and control simulation techniques applicable to large space structures, encompassing the model of the large structure as well as models of its dynamics, its onboard controller, its sensor/actuator systems, and various disturbances to which it may be subjected. Control performance parameters must be computed as functions of time, or of such other design parameters as control gain. A large space antenna is used as an example of the structures in question, illustrating the way in which an efficient dynamics and control simulation structure program can be developed, and how antenna parameters such as reflector surface distortions can be computed, without having to solve a large number of equations for each computation time interval.
Document ID
19850066858
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, Y. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cameron, J.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Aerospace simulation
Location: San Diego, CA
Start Date: February 2, 1984
End Date: February 4, 1984
Accession Number
85A49009
Distribution Limits
Public
Copyright
Other

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