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Computer simulation of a resonant dc link for advanced launch systemsThe performance of a resonant dc link based actuator power system being built for an advanced launch system application is evaluated for a typical launch scenario using two end-to-end system simulations, one using a digital computer and the other using a hybrid computer. Aspects of system performance from the switching of the power electronic devices to the vehicle aerodynamics are addressed. Using these simulations, it is shown that the resonance dc link actuator adequately stabilize the vehicle against a wind gust during a launch.
Document ID
19950062084
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sudhoff, S. D. (NASA Lewis Research Center Cleveland, OH, United States)
Wasynczuk, O. (NASA Lewis Research Center Cleveland, OH, United States)
Krause, P. C. (NASA Lewis Research Center Cleveland, OH, United States)
Kenny, B. H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
ISSN: 0148-7191
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SAE PAPER 931424
Report Number: SAE PAPER 931424
ISSN: 0148-7191
Meeting Information
Meeting: SAE, Aerospace Atlantic Conference & Exposition
Location: Dayton, OH
Country: United States
Start Date: April 20, 1993
End Date: April 23, 1993
Accession Number
95A93683
Distribution Limits
Public
Copyright
Other

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