NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Obstacles to high fidelity multibody dynamics simulationThe authors take a wide ranging look at issues involved in the dynamic modeling of complex, multibodied orbiting space systems. The nature of the multibody problem is reviewed and capabilities and limitations of two major codes (DISCOS, TREETOPS) are assessed. Problem areas that limit accuracy or contribute to uncertainty in the modeling, simulation process are identified. As a specific case, the significance of including, or of not including, second-degree geometric nonlinearity in the elastic displacement field (foreshortening) is evaluated. Conclusions and recommendations are made concerning the direction future development should take to achieve higher-fidelity and more computationally efficient multibody software solutions.
Document ID
19880067244
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lips, K. W.
(Honeywell, Inc. Space and Strategic Avionics Div., Clearwater, FL, United States)
Singh, R. P.
(DYNACS Engineering Co., Inc. Clearwater, FL, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 1988 American Control Conference
Location: Atlanta, GA
Country: United States
Start Date: June 15, 1988
End Date: June 17, 1988
Accession Number
88A54471
Funding Number(s)
CONTRACT_GRANT: NAS8-34588
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available