Andy J. Keane

ORCID: 0000-0001-7993-1569
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About
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Research Areas
  • Advanced Multi-Objective Optimization Algorithms
  • Probabilistic and Robust Engineering Design
  • Manufacturing Process and Optimization
  • X-ray Diffraction in Crystallography
  • Crystallization and Solubility Studies
  • Optimal Experimental Design Methods
  • Advanced Aircraft Design and Technologies
  • Metaheuristic Optimization Algorithms Research
  • Turbomachinery Performance and Optimization
  • Topology Optimization in Engineering
  • Acoustic Wave Phenomena Research
  • Evolutionary Algorithms and Applications
  • Structural Health Monitoring Techniques
  • Distributed and Parallel Computing Systems
  • Computational Fluid Dynamics and Aerodynamics
  • Structural Analysis and Optimization
  • Advanced Numerical Analysis Techniques
  • Vibration and Dynamic Analysis
  • Scientific Computing and Data Management
  • Aerospace and Aviation Technology
  • Wind and Air Flow Studies
  • Parallel Computing and Optimization Techniques
  • Model Reduction and Neural Networks
  • Aeroelasticity and Vibration Control
  • Crystallography and molecular interactions

University of Southampton
2015-2025

Rolls-Royce (United Kingdom)
2007-2022

University College Cork
2021

Airbus (United Kingdom)
2018

University of Maryland, College Park
2011-2015

Brunel University of London
1987-2014

IBAT College
2012

Technology Partnership (United Kingdom)
2007

Google (United States)
2006-2007

University of Oxford
1991-1996

10.1016/j.paerosci.2008.11.001 article EN Progress in Aerospace Sciences 2009-01-01

This paper demonstrates the application of correlated Gaussian process based approximations to optimization where multiple levels analysis are available, using an extension geostatistical method co-kriging . An exchange algorithm is used choose which points search space sample within each level analysis. The derivation equations presented in intuitive manner, along with a new variance estimator account for varying degrees computational ‘noise’ A multi-fidelity wing demonstrate methodology.

10.1098/rspa.2007.1900 article EN Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences 2007-10-02

Over the last decade, memetic algorithms (MAs) have relied on use of a variety different methods as local improvement procedure. Some recent studies choice search method employed shown that this significantly affects efficiency problem searches. Given restricted theoretical knowledge available in area and limited progress made mitigating effects incorrect choice, we present strategies for MA control decide, at runtime, which is chosen to locally improve next chromosome. The multiple during...

10.1109/tevc.2003.819944 article EN IEEE Transactions on Evolutionary Computation 2004-04-01

We present a parallel evolutionary optimization algorithm that leverages surrogate models for solving computationally expensive design problems with general constraints, on limited computational budget. The essential backbone of our framework is an coupled feasible sequential quadratic programming solver in the spirit Lamarckian learning. employ trust-region approach interleaving use exact modelsfortheobjectiveandconstraintfunctionswithcomputationallycheapsurrogatemodelsduringlocalsearch. In...

10.2514/2.1999 article EN AIAA Journal 2003-04-01

In this paper, we present a novel surrogate-assisted evolutionary optimization framework for solving computationally expensive problems. The proposed uses cheap hierarchical surrogate models constructed through online learning to replace the exact objective functions during search. At first level, employs data-parallel Gaussian process based global model filter algorithm (EA) population of promising individuals. Subsequently, these potential individuals undergo memetic search in form...

10.1109/tsmcc.2005.855506 article EN IEEE Transactions on Systems Man and Cybernetics Part C (Applications and Reviews) 2006-12-19

Design of experiment and response surface modeling methods are applied to the problem constructing Pareto fronts for computationally expensive multiobjective design optimization problems. The work presented combines with kriging (Gaussian process) models enable parallel evolution sets. This is achieved via use updating schemes based on new extensions expected improvement criterion commonly in single-objective searches. approaches described provide a statistically coherent means solving...

10.2514/1.16875 article EN AIAA Journal 2006-04-01

of functions calculated by long running computer codes. The literature in this area commonly assumes that the objective function is a smooth, deterministic inputs. Yet it well known many simulations,especiallythoseofcomputational fluidandstructuraldynamicscodes,oftendisplaywhatonemightcall numerical noise: rather than lying on smooth curve, results appear to contain random scatter about trend. This paper extends previous optimization methods based interpolating method ofkriging case such...

10.2514/1.20068 article EN AIAA Journal 2006-10-01

Efficient methods for global aerodynamic optimization using computational fluid dynamics simulations should aim to reduce both the time taken evaluate design concepts and number of evaluations needed optimization. This paper investigates improving such efficiency through use partially converged results. These allow surrogate models be built in a fraction required based on The proposed methodologies increase speed convergence optimum while computer resources expended areas poor designs are...

10.1098/rspa.2006.1679 article EN Proceedings of the Royal Society A Mathematical Physical and Engineering Sciences 2006-03-06

This article discusses the benefits of different infill sampling criteria used in surrogate-based constrained global optimization. A new method which selects multiple updates based on Pareto optimal solutions is introduced showing improvements over a number existing methods. The construction surrogates (also known as meta-models or response surface models) involves selection limited designs are analysed using original expensive functions. typical approach two stages. First surrogate built an...

10.1080/0305215x.2011.637556 article EN Engineering Optimization 2012-02-08

Response surfaces have been extensively used as a method of building effective surrogate models high-fidelity computational simulations. Of the numerous types response surface models, kriging is perhaps one most effective, due to its ability model complicated responses through interpolation or regression known data while providing an estimate error in prediction. There is, however, little information indicating extent which hyperparameters need be tuned for resulting effective. The following...

10.2514/1.34822 article EN AIAA Journal 2008-04-10

A highly efficient and versatile chemical cycle has been developed for the production of isocyanates through molecular fixation N2 , CO2 R3 ECl (E=C, Si, Ge). Key steps include a 'one-pot' photolytic N-N bond cleavage Group 6 dinuclear dinitrogen complex with in situ trapping by to provide metal terminal imido that can engage simultaneous nitrene-group transfer oxygen-atom generate an intermediate oxo release isocyanate product. Reaction additional equivalents regenerates dichloride is...

10.1002/anie.201502293 article EN Angewandte Chemie International Edition 2015-06-26

An empirical drag prediction model plus design of experiment, response surface, and data-fusionmethods are brought together with computational fluid dynamics (CFD) to provide a wing optimization system. This system allows high-quality designs be found using full three-dimensional CFD code without the expense direct searches. The metamodels built shown more accurate than initial or simple surfaces based on data alone. Data fusion is achieved by building surface kriging differences between two...

10.2514/2.3153 article EN Journal of Aircraft 2003-07-01

When carrying out design searches, traditional variable screening techniques can find it extremely difficult to distinguish between important and unimportant variables. This is particularly true when only a small number of simulations combined with parameterization which results in large variables seemingly equal importance. Here the authors present reduction technique employs proper orthogonal decomposition filter undesirable or badly performing geometries from an optimization process....

10.2514/1.41420 article EN AIAA Journal 2010-04-12

Multipoint objective functions are often employed within aerodynamic optimizations to prevent a reduction in offdesign performance. However, this typically results the need for significant number of simulations at variety design conditions calculate function. The following paper attempts address problem through application multilevel cokriging model optimization process. A large single-point augmented by smaller multipoint simulations. technique is shown result surrogate models as effective...

10.2514/1.c031342 article EN Journal of Aircraft 2011-09-01

Experimental data support a mechanism for N≡N bond cleavage within series of group 5 bimetallic dinitrogen complexes general formula, {Cp*M[N((i)Pr)C(R)N((i)Pr)]}2(μ-N2) (Cp* = η(5)-C5Me5) (M Nb, Ta), that proceeds in solution through an intramolecular "end-on-bridged" (μ-η(1):η(1)-N2) to "side-on-bridged" (μ-η(2):η(2)-N2) isomerization process quantitatively provide the corresponding bis(μ-nitrido) complexes, {Cp*M[N((i)Pr)C(R)N((i)Pr)](μ-N)}2. It is further demonstrated subtle changes...

10.1021/ja505309j article EN Journal of the American Chemical Society 2014-06-24

Stochastic reduced basis methods for solving large-scale linear random algebraic systems of equations, such as those obtained by discretizing stochastic partial differential equations in space, time, and the dimension, are introduced. The fundamental idea employed is to represent system response using a combination vectors with undetermined deterministic coefficients (or functions). We present theoretical justification employing spanning preconditioned Krylov subspace approximate process....

10.2514/2.1837 article EN AIAA Journal 2002-08-01
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