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A Historical Perspective on Dynamics Testing at the Langley Research CenterThe experience and advancement of Structural dynamics testing for space system applications at the Langley Research Center of the National Aeronautics and Space Administration (NASA) over the past four decades is reviewed. This experience began in the 1960's with the development of a technology base using a variety of physical models to explore dynamic phenomena and to develop reliable analytical modeling capability for space systems. It continued through the 1970's and 80's with the development of rapid, computer-aided test techniques, the testing of low-natural frequency, gravity-sensitive systems, the testing of integrated structures with active flexible motion control, and orbital flight measurements, It extended into the 1990's where advanced computerized system identification methods were developed for estimating the dynamic states of complex, lightweight, flexible aerospace systems, The scope of discussion in this paper includes ground and flight tests and summarizes lessons learned in both successes and failures.
Document ID
20000046786
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Horta, Lucas G.
(NASA Langley Research Center Hampton, VA United States)
Kvaternik, Raymond G.
(NASA Langley Research Center Hampton, VA United States)
Hanks, Brantley R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
April 6, 2000
Subject Category
General
Report/Patent Number
AIAA Paper 2000-1739
Report Number: AIAA Paper 2000-1739
Meeting Information
Meeting: Dynamics Specialist Conference
Location: Atlanta, GA
Country: United States
Start Date: April 3, 2000
End Date: April 6, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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