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Modeling, system identification, and control of ASTREXThe modeling, system identification and controller design aspects of the ASTREX precision space structure are presented in this work. Modeling of ASTREX is performed using NASTRAN, TREETOPS and I-DEAS. The models generated range from simple linear time-invariant models to nonlinear models used for large angle simulations. Identification in both the time and frequency domains are presented. The experimental set up and the results from the identification experiments are included. Finally, controller design for ASTREX is presented. Simulation results using this optimal controller demonstrate the controller performance. Finally the future directions and plans for the facility are addressed.
Document ID
19930009753
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abhyankar, Nandu S.
(DYNACS Engineering Co., Inc. Palm Harbor, FL, United States)
Ramakrishnan, J.
(DYNACS Engineering Co., Inc. Palm Harbor, FL, United States)
Byun, K. W.
(DYNACS Engineering Co., Inc. Palm Harbor, FL, United States)
Das, A.
(Phillips Lab. Edwards AFB, CA., United States)
Cossey, Derek F.
(Phillips Lab. Edwards AFB, CA., United States)
Berg, J.
(Phillips Lab. Edwards AFB, CA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, The Fifth NASA(DOD Controls-Structures Interaction Technology Conference, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N18942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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