2016
DOI: 10.3233/ica-160529
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Covariance matrix adaptation pareto archived evolution strategy with hypervolume-sorted adaptive grid algorithm

Abstract: Abstract. Real-world problems often involve the optimisation of multiple conflicting objectives. These problems, referred to as multi-objective optimisation problems, are especially challenging when more than three objectives are considered simultaneously. This paper proposes an algorithm to address this class of problems. The proposed algorithm is an evolutionary algorithm based on an evolution strategy framework, and more specifically, on the Covariance Matrix Adaptation Pareto Archived Evolution Strategy (C… Show more

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Cited by 69 publications
(30 citation statements)
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“…This paper proposes a novel progressive preference articulation mechanism for multi-objective optimisation problems. Furthermore, this mechanism is incorporated into an optimisation framework recently proposed in the literature, namely the Covariance Matrix Adaptation Pareto Archived Evolution Strategy with Hypervolume-sorted Adaptive Grid Algorithm (CMA-PAES-HAGA), see [50]. The resulting algorithm has been thoroughly tested and compared against modern algorithms which implicitly and explicitly incorporate preference articulation.…”
Section: Progressive Preference Articulation: a Brief Reviewmentioning
confidence: 99%
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“…This paper proposes a novel progressive preference articulation mechanism for multi-objective optimisation problems. Furthermore, this mechanism is incorporated into an optimisation framework recently proposed in the literature, namely the Covariance Matrix Adaptation Pareto Archived Evolution Strategy with Hypervolume-sorted Adaptive Grid Algorithm (CMA-PAES-HAGA), see [50]. The resulting algorithm has been thoroughly tested and compared against modern algorithms which implicitly and explicitly incorporate preference articulation.…”
Section: Progressive Preference Articulation: a Brief Reviewmentioning
confidence: 99%
“…In accordance with the notation used in the field, the parent population size is indicated with µ while the offspring population size is indicated with λ , see [50]. As shown in the following subsections, the µ parent solutions generate λ offspring solutions at each generation, and µ solutions must then be selected from the N = µ + λ solutions in X.…”
Section: Background -Notationmentioning
confidence: 99%
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“…More details about this aircraft dynamic model can be found in [58][59][60]. To handle the constraints, the penalty function which was presented in [61] is used.…”
Section: Flight Dynamic Control Optimisation Problemmentioning
confidence: 99%
“…In this work, only the lateral/ directional motion control is considered. A state equation representing the dynamic motion of an aircraft is expressed as follows [57][58][59][60] where x = { , , , } , is the sideslip, a velocity in direction, is the yaw rate, rate of change of rotation about the -axis, is the roll rate, rate of change of rotation about the -axis, is the bank angle, rotation about the -axis, A is the kinetic energy matrix, B is Coriolis matrix, u = { } is the control vector, is the aileron deflection, and is the rudder deflection.…”
Section: Flight Dynamic Control Optimisation Problemmentioning
confidence: 99%