Evidence-based preliminary design of spacecraft
Alicino, Simone and Vasile, Massimiliano (2014) Evidence-based preliminary design of spacecraft. In: 6th International Conference on Systems & Concurrent Engineering for Space Applications. SECESA 2014, 2014-10-08 - 2014-10-10.
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Abstract
This paper presents a computational tool that has been specifically developed for evidence-based robust design problems. The paper starts with a brief overview of evidence theory and its use in system design. Then a tool to reduce the computational cost of computing the Belief and Plausibility is discussed. The tool is composed of an evolutionary algorithm for worst-case scenario optimization, and a decomposition technique applicable to space systems engineering. Finally, a test case of the preliminary design of a small spacecraft will illustrate the results of the evidence-based robust design optimization in comparison to the margin approach.
ORCID iDs
Alicino, Simone ORCID: https://orcid.org/0000-0002-0213-7719 and Vasile, Massimiliano ORCID: https://orcid.org/0000-0001-8302-6465;-
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Item type: Conference or Workshop Item(Paper) ID code: 52252 Dates: DateEventOctober 2014PublishedNotes: Date of Acceptance: 22/07/2014 Subjects: Technology > Mechanical engineering and machinery
Technology > Motor vehicles. Aeronautics. AstronauticsDepartment: Faculty of Engineering > Mechanical and Aerospace Engineering
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Pure Administrator Date deposited: 18 Mar 2015 10:57 Last modified: 11 Nov 2024 16:42 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/52252