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Shuttle flight control and structure interactionA brief overview of the (DAP) Dynamic Autopilot is given. Results of the dynamic interaction study of the Orbiter with the General Dynamics Beam are presented. Preliminary results of the three degree of freedom payload parametric study are also presented.
Document ID
19830014002
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Paluszek, M. (Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1983
Publication Information
Publication: NASA. Langley Research Center Structural Dyn. and Control of Large Space Struct., 1982
Subject Category
Space Transportation
Accession Number
83N22273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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