DocumentCode :
1937813
Title :
FRACSAT: Automated design synthesis for future space architectures
Author :
Mackey, R. ; Uckun, S. ; Minh Do ; Shah, J.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2013
fDate :
2-9 March 2013
Firstpage :
1
Lastpage :
12
Abstract :
This paper describes the algorithmic basis and development of FRACSAT (FRACtionated Spacecraft Architecture Toolkit), a new approach to conceptual design, cost-benefit analysis, and detailed trade studies for space systems. It provides an automated capability for exploration of candidate spacecraft architectures, leading users to near-optimal solutions with respect to user-defined requirements, risks, and program uncertainties. FRACSAT utilizes a sophisticated planning algorithm (PlanVisioner) to perform a quasi-exhaustive search for candidate architectures, constructing candidates from an extensible model-based representation of space system components and functions. These candidates are then evaluated with emphasis on the business case, computing the expected design utility and system costs as well as risk, presenting the user with a greatly reduced selection of candidates. The user may further refine the search according to cost or benefit uncertainty, adaptability, or other performance metrics as needed.
Keywords :
costing; risk analysis; space vehicles; systems engineering; FRACSAT; PlanVisioner; automated design synthesis; benefit uncertainty; cost uncertainty; cost-benefit analysis; fractionated spacecraft architecture toolkit; near-optimal solutions; planning algorithm; program uncertainty; quasiexhaustive search; risk uncertainty; space system components; space system functions; spacecraft architectures exploration; user-defined requirements; Algorithm design and analysis; Computer architecture; Libraries; Measurement; Planning; Space vehicles; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4673-1812-9
Type :
conf
DOI :
10.1109/AERO.2013.6497169
Filename :
6497169
Link To Document :
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