DocumentCode
487294
Title
Obstacles to High Fidelity Multibody Dynamics Simulation
Author
Lips, K.W. ; Singh, R.P.
Author_Institution
Honeywell, Inc. Space & Strategic Avionics Division, Clearwater, Florida
fYear
1988
fDate
15-17 June 1988
Firstpage
587
Lastpage
594
Abstract
This study takes 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, 2nd degree geometric nonlinearity in the elastic displacement field (foreshortening) is evaluated Conclusion and recommendations are made concerning the direction future development should take in order to achieve higher fidelity, more computationally efficient multibody software solutions.
Keywords
Aerospace electronics; Antenna measurements; Control design; Equations; Extraterrestrial measurements; Lips; Physics; Sorting; Space vehicles; Spaceborne radar;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1988
Conference_Location
Atlanta, Ga, USA
Type
conf
Filename
4789787
Link To Document