2019
DOI: 10.1007/s12008-019-00590-7
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Interactive design and multidisciplinary optimization of geostationary communication satellite

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Cited by 15 publications
(7 citation statements)
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References 30 publications
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“…7 shows two design variants with different hub knee radial positions (hk_radial), thus causing different laser beam incident angles (α=10.6• and α=18. 3…”
Section: Identifying Producibility Features (A)-figmentioning
confidence: 99%
See 1 more Smart Citation
“…7 shows two design variants with different hub knee radial positions (hk_radial), thus causing different laser beam incident angles (α=10.6• and α=18. 3…”
Section: Identifying Producibility Features (A)-figmentioning
confidence: 99%
“…Multidisciplinary Design Optimization (MDO) approaches in the aerospace industry involve trade-offs between various engineering disciplines for the objective of reducing mass, fuel consumption, manufacturing costs and emissions while increasing product performance [1]. The automation of the analysis and optimization activities within the MDO process of aerospace products is constantly under development [1][2][3]. Over the last few years, MDO approaches have benefitted from the maturation of computer-aided modeling, automation and statistical techniques, which have made possible the efficient evaluation and optimization of the performance of a large number of design variants [2,[4][5][6][7].…”
Section: Introductionmentioning
confidence: 99%
“…Each of these variables need to be considered throughout the design lifecycle of the satellite. To illustrate the usefulness of GAs in this context, Berrezzoug et al [17] proposed a method which applies a Gravitational Search Algorithm to the design of a satellite by considering the many design variables. The approach proved useful for determining optimal trade-offs between the variables.…”
Section: A Genetic Algorithmsmentioning
confidence: 99%
“…The CD analysis of complex space systems is typically performed by a multidisciplinary process for designing the system by modelling and integrating its constituting subsystems [45]. The subsystems are modelled through physics-based parametric equation analysis [6] and numerous design synthesis tools have been developed to support the design space exploration and analysis [18,34,38,48,49]. Over the years, numerous design process would drive the analysis of various spacecraft subsystems separately whereas information is passed from one subsystem to other in a sequential manner.…”
Section: Introductionmentioning
confidence: 99%