Rapid Trajectory Optimization Using Computational Intelligence for Guidance and Conceptual Design of Multistage Space Launch Vehicles
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics
2. R&D Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6062
Reference18 articles.
1. Hammond,W.E.,DesignMethodologiesforSpaceTransportationSystems,AIAA,Reston,VA,2001.
2. Sobieszczanski-Sobieski, J., and Haftka, R. T. "Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments,"AIAA Paper 96-0711, Jan. 1996.
3. TRANSYS - Space Transportation System preliminary design software
4. Design feasibility via ascent optimality for next-generation spacecraft
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