DocumentCode
2113131
Title
Model-based engineering design for space missions
Author
Wall, STEPHEN D.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
6
fYear
2004
fDate
6-13 March 2004
Firstpage
3907
Abstract
The basic elements of model-based design for space missions have existed for almost a decade, awaiting an opportunity to implement them in the same place at the same time. In early design phases, combinations of models, concurrent engineering methods, and scenario-driven design have been used for several years with results that have exceeded even optimistic expectations; but the goal of extending these methods to later phases of design has been more elusive. JPL´s model-based engineering design (MBED) initiative provides opportunity to reach that goal. It enables advanced systems engineering practice through a series of integrated, increasingly detailed models that provide continuity from architectural concept through detailed design. It extends current capability for rapid conceptual design, allowing thorough exploration of design tradespaces and selection of an optimal design point with associated cost and rationale; and it provides seamless connection to subsystem models and detailed design tool suites. We review the goals and status of MBED and show the expected interconnectivity between conceptual and detailed design.
Keywords
aerospace engineering; aerospace simulation; concurrent engineering; design engineering; space vehicles; systems engineering; advanced systems engineering; concurrent engineering methods; design tradespaces; model based engineering design; optimal design point; rapid conceptual design; scenario driven design; space missions; subsystem models; Concurrent engineering; Design engineering; Design methodology; Engineering management; Laboratories; Process design; Productivity; Propulsion; Space missions; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1368208
Filename
1368208
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