RLV reentry trajectory multi-objective optimization design based on NSGA-II algorithm

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2005, Pages 1054-1059

  Gang, Chen ^a,c   Min, Xu ^a,c   Zi ming, Wan ^b,c   Si lu, Chen ^a,c,d  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b Institute of Chinese Defense Technology   (China)

^c Department of Flight Vehicle Design ^*

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT-HANDLING STRATEGY; OPTIMAL TRAJECTORY; OPTIMIZATION PROBLEMS; WEIGHTING FACTOR;

OPTIMIZATION; PROBLEM SOLVING; THERMAL LOAD; TRAJECTORIES;

ALGORITHMS;

EID: 29344440302     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Hu Yu-da. Practical multi-objective programming. Shanghai technology and Science Press, 1990.
2. Deb K, Pratap A, Agarwal S, et al. A Fast and Elitist Multi-Objective Genetic Algorithm: NSGA-II[R]. KanGAL Report No.200001, 2000.
3. Hartmann,J W, Coverstone-Carroll,V L, Williams, S N.Optimal Interplanetary spacecraft Trajectores via a Pareto Genetic Algorithm. The Journal of the Astronautical Sciences,1998,46(3):267-282.
4. Srinivas N, Deb K. Multi-objective Function Optimization Using Non-dominated Sorting Genetical Algorithms[J]. Evolutionary Computation, 1995, 2(3): 221-248.
5. Arora R K. Reentry Trajectory Optimization: Evolutionary Approach[R]. AIAA-2002-5466, 2002.
6. Chen Gang, Wan Zi-ming, Xu Min and Chen Si-lu. Overview of the Application of Genetic Algorithm in Craft Trajectory Optimizaton. Journal of Ballistics, to be print.