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Control/structure interaction design methodologyThe Control Structure Interaction Program is a technology development program for spacecraft that exhibit interactions between the control system and structural dynamics. The program objectives include development and verification of new design concepts (such as active structure) and new tools (such as a combined structure and control optimization algorithm) and their verification in ground and possibly flight test. The new CSI design methodology is centered around interdisciplinary engineers using new tools that closely integrate structures and controls. Verification is an important CSI theme and analysts will be closely integrated to the CSI Test Bed laboratory. Components, concepts, tools and algorithms will be developed and tested in the lab and in future Shuttle-based flight experiments. The design methodology is summarized in block diagrams depicting the evolution of a spacecraft design and descriptions of analytical capabilities used in the process. The multiyear JPL CSI implementation plan is described along with the essentials of several new tools. A distributed network of computation servers and workstations was designed that will provide a state-of-the-art development base for the CSI technologies.
Document ID
19900013737
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Briggs, Hugh C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Layman, William E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 15, 1989
Publication Information
Publication: Proceedings of the 3rd Annual Conference on Aerospace Computational Control, Volume 2
Subject Category
Computer Programming And Software
Accession Number
90N23053
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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