% For a description of the spacecraft trajectory problem and links % to the problem instances see (Vinko_et_al:2007) global MGADSMproblem cd ..\Trajectory load EdEdJ % This instance can be downloaded from the ESA web page NumbVar = 12; PopSize = 1000; F = 'EvalSaga'; % The function should be modified to enforce maximization, i.e g(x) = -1*f(x) Card(1,:) = [7000,0,0,0,50,300,0.01,0.01,1.05,8,-1*pi,-1*pi]; Card(2,:) = [9100,7,1,1,2000,2000,0.90,0.90,7.00,500,pi,pi]; cache = [0,0,0,0,0]; learning_params(1:5) = {'vars','ClusterPointsKmeans',10,'sqEuclidean',1}; edaparams{1} = {'learning_method', |