RLV Reentry Trajectory Multi-Objective Optimization Design Based on NSGA2 Algorithm
Author:
Affiliation:
1. Northwestern Polytechnical University
2. Institute of Chinese Defense Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6131
Reference5 articles.
1. Deb K , Pratap A, Agarwal S, etal. A Fast and Elitist Multi-Objective Genetic Algorithm: NSGA-II[R]. KanGAL Report No.200001,2000.
2. Optimal Interplanetary Spacecraft Trajectories via a Pareto Genetic Algorithm
3. AroraR K. ReentryTrajectoryOptimization: EvolutionaryApproach[R]. AIAA-2002-5466,2002.
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