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A generic multi-flex-body dynamics, controls simulation tool for space stationAn order (n) multiflex body Space Station simulation tool is introduced. The flex multibody modeling is generic enough to model all phases of Space Station from build up through to Assembly Complete configuration and beyond. Multibody subsystems such as the Mobile Servicing System (MSS) undergoing a prescribed translation and rotation are also allowed. The software includes aerodynamic, gravity gradient, and magnetic field models. User defined controllers can be discrete or continuous. Extensive preprocessing of 'body by body' NASTRAN flex data is built in. A significant aspect, too, is the integrated controls design capability which includes model reduction and analytic linearization.
Document ID
19910013008
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
London, Ken W.
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Lee, John F.
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Singh, Ramen P.
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Schubele, Buddy
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N22321
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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