Enhanced Hybrid Differential Evolution for Earth-Moon Low-Energy Transfer Trajectory Optimization
Algorithm 1: DE/rand/1/exp.
1: Generate the initial population , define as the -th individual in , is the population size, is the number of function evaluations in each run, MaxNFEs is the number of max function evaluation, is the number of decision variable, is the mutation factor, is crossover rate.
2:
3: Evaluate the fitness for the each individual in .