An approach for the robust design of the power systems of small satellites
Vasile, Massimiliano and Alicino, Simone (2014) An approach for the robust design of the power systems of small satellites. In: 65th International Astronautical Congress (IAC 2014), 2014-09-29 - 2014-10-03, Toronto. (Unpublished)
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The paper presents an approach to Robust Model-Based System Engineering (RMBSE) applied to the design of the power system of a small-satellite. Tow simple low-fidelity parametric models of the power and telecommunication systems are used to compute the mass and power requirements for different orbital geometries. The low model fidelity implies that model and parameters are affected by epistemic uncertainty. This uncertainty is commonly captured by adding margins at subsystem and system level. In this paper instead, the effect of epistemic uncertainty is modelled with p-boxes on finite sets of values and propagated through the system models to compute the upper and lower expectation on the mass budget. A robust optimisation procedure is then introduced to find the design solution that minimises system mass and the impact of uncertainty.
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Item type: Conference or Workshop Item(Paper) ID code: 50600 Dates: DateEventOctober 2014PublishedKeywords: robust design, power systems, small satellites, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering Subjects: Technology > Motor vehicles. Aeronautics. Astronautics Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Technology and Innovation Centre > Advanced Engineering and ManufacturingDepositing user: Pure Administrator Date deposited: 27 Nov 2014 16:17 Last modified: 27 Nov 2014 16:17 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/50600