2014
DOI: 10.5028/jatm.v6i1.288
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Theoretical Optimal Trajectories for Reducing the Environmental Impact of Commercial Aircraft Operations

Abstract: This work describes initial results obtained from an ongoing research involving the development of optimization algorithms which are capable of performing multi-disciplinary aircraft trajectory optimization processes. A short description of both the rationale behind the initial selection of a suitable optimization technique and the status of the optimization algorithms is firstly presented. The optimization algorithms developed are subsequently utilized to analyze different case studies involving one or more f… Show more

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Cited by 18 publications
(17 citation statements)
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“…the NO x emission by 0.3 %pt, whereas this option increases flight time by 0.2 %pt and fuel use by 0.2 %pt, compared to those measures of the fuel option Celis et al (2014). addressed a single-objective flight trajectory optimization on total fuel use and on NO x emission, respectively, with the same simulation setup described above.…”
mentioning
confidence: 99%
“…the NO x emission by 0.3 %pt, whereas this option increases flight time by 0.2 %pt and fuel use by 0.2 %pt, compared to those measures of the fuel option Celis et al (2014). addressed a single-objective flight trajectory optimization on total fuel use and on NO x emission, respectively, with the same simulation setup described above.…”
mentioning
confidence: 99%
“…Also, they are tolerant of noise in the objective function and have no difficulty with categorical variable changes [20]. In addition, GAs can explore the solution space in multiple directions at once, hence increasing the chance of finding the optimal solution [21]. Also, GA is robust in locating optimal solution and reducing the computational effort than other conventional heuristics [20].…”
Section: Methodology: Gas As An Optimization Tool For Mtowmentioning
confidence: 99%
“…The set of altitudes and speeds that compose a flight is called the vertical reference trajectory. Algorithms optimizing the vertical reference trajectory have been developed by using Optimal control [15][16][17][18][19], Mixed-Integer Linear Programming [20,21], and Dynamic Programming [22,23]. Most of these techniques use the point-mass equations of motion and the BADA database provided by Eurocontrol to compute the aircraft fuel burn.…”
Section: Introductionmentioning
confidence: 99%