Referenced Items are not available for this document.
The application of optimization to spacecraft design has the potential to significantly improve decision-making capabilities early in the design process. Successful integration of optimization and system-level spacecraft tools allow the concept architecture, technology choices, and performance requirements to be adjusted to meet an overall estimated cost goal; thereby enabling spacecraft design to be completed in a reliable, economical and timely manner
Published in:
Aerospace Conference Proceedings, 2000 IEEE
(Volume:1
)
Date of Conference: 2000
- Page(s):
- 371 - 384 vol.1
- Meeting Date :
- 18 Mar 2000-25 Mar 2000
- ISSN :
- 1095-323X
- Print ISBN:
- 0-7803-5846-5
- INSPEC Accession Number:
- 6763015
- Conference Location :
- Big Sky, MT
- Digital Object Identifier :
- 10.1109/AERO.2000.879413
- Product Type:
- Conference Publications
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