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Optimal Trajectory & Configuration of Commuter Aircraft with Stochastic and Gradient based Methods

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Progress in Industrial Mathematics at ECMI 96

Part of the book series: European Consortium for Mathematics in Industry ((ECMI,volume 9))

Abstract

This paper discusses the application of two stochastic optimization methods viz. Simulated Annealing (SA) and Genetic Algorithms (GA) in conceptual design of commuter aircraft. Brief description of a methodology for integrated trajectory and configuration optimization of commuter aircraft is provided, along with the three different objective functions. The features of SIMANN SA algorithm and GOOD GA program are then outlined. The results obtained with these two techniques are compared with those obtained with a proprietary gradient search procedure RQPMIN for all the three objective functions. It was seen that SIMANN & GOOD come up with similar or better configurations compared to RQPMIN. While SIMANN & GOOD required much larger number of evaluations per run compared to RQPMIN, they were found to be less prone to getting trapped in the local minima.

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© 1997 B. G. Teubner Stuttgart

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Pant, R., Kalker-Kalkman, C.M. (1997). Optimal Trajectory & Configuration of Commuter Aircraft with Stochastic and Gradient based Methods. In: Brøns, M., Bendsøe, M.P., Sørensen, M.P. (eds) Progress in Industrial Mathematics at ECMI 96. European Consortium for Mathematics in Industry, vol 9. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-96688-9_39

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  • DOI: https://doi.org/10.1007/978-3-322-96688-9_39

  • Publisher Name: Vieweg+Teubner Verlag, Wiesbaden

  • Print ISBN: 978-3-322-96689-6

  • Online ISBN: 978-3-322-96688-9

  • eBook Packages: Springer Book Archive

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