Abstract

In an effort to allow to increase the number of aircraft and airport operations while mitigating their negative impacts (e.g., noise and pollutant emission) on near-airport communities, the optimal design of new departure routes with less noise and fuel consumption becomes more important. In this paper, a multi-objective evolutionary algorithm based on decomposition (MOEA/D), which recently emerged as a potential method for solving multi-objective optimization problems (MOPs), is developed for this kind of problem. First, to minimize aircraft noise for departure routes while taking into account the interests of various stakeholders, bi-objective optimization problems involving noise and fuel consumption are formulated where both the ground track and vertical profile of a departure route are optimized simultaneously. Second, in order to make the design space of vertical profiles feasible during the optimization process, a trajectory parameterization technique recently proposed is employed. Furthermore, some modifications to MOEA/D that are aimed at significantly reducing the computational cost are also introduced. Two different examples of departure routes at Schiphol Airport in the Netherlands are shown to demonstrate the applicability and reliability of the proposed method. The simulation results reveal that the proposed method is an effective and efficient approach for solving this kind of problem.

Highlights

  • Due to the high demand of air transport, the aviation industry is expected to develop rapidly in the coming years [1]

  • 3, it can be that the quality of solutions obtained by multi-objective evolutionary algorithm based on decomposition (MOEA/D) is generally better than those achieved by NSGA-II

  • MOEA/D isunderneath an effectivea during which an aircraft at aobtained low attitude depends population method for solving the optimal design problem of noise abatement departure routes

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Summary

Introduction

Due to the high demand of air transport, the aviation industry is expected to develop rapidly in the coming years [1]. From the obtained results in [18,19,20], it is clear that the use of non-gradient multi-objective optimization methods is a potential approach for designing new routes These methods readily overcome the limitations of gradient-based methods in dealing with discontinuous problems and integer or discrete design variables and can find out a set of non-dominated optimal solutions, which helps to present more options to policymakers and authorities. Because they feature random searches with multiple design points at the same time, these methods require many evaluations of the objective and constraint functions which are quite time-consuming These restrictions again have motivated researchers to develop computationally efficient approaches that can balance the expected results and computation cost effectively.

Aircraft Model
Formulation of the Optimization Problem
New Implementations
Numerical Example
The cases inFigure
Compared
Despite
Departure
Optimal ground ground tracks obtained obtained by NSGA-II
Conclusions
Findings
Visser
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