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The LISA Integrated ModelThe Laser Interferometer Space Antenna (LISA) space mission has unique needs that argue for an aggressive modeling effort. These models ultimately need to forecast and interrelate the behavior of the science input, structure, optics, control systems, and many other factors that affect the performance of the flight hardware. In addition, many components of these integrated models will also be used separately for the evaluation and investigation of design choices, technology development and integration and test. This article presents an overview of the LISA integrated modeling effort.
Document ID
20030032361
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Merkowitz, Stephen M. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: LISA Symposium
Location: PA
Country: United States
Start Date: July 19, 2002
End Date: July 24, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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