Support Vector Machine Based Trajectory Metamodel for Conceptual Design of Multi-stage Space Launch Vehicle-Reference-Cited by-同舟云学术

Support Vector Machine Based Trajectory Metamodel for Conceptual Design of Multi-stage Space Launch Vehicle

Published:2005 Issue: Volume: Page:528-535
ISSN:0302-9743
Container-title:Computational Intelligence and Security
language:
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Author:

Akhtar Saqlain,Linshu He

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/11596448_77.pdf

Reference7 articles.

1. Martin, J., Alonso, J.J.: Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method. In: 9th AIAA/ISSMO, 2002–5402, Atlanta, GA (2002)

2. Tsuchiya, T., Mori, T.: Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles including Trajectory Optimization. Journal of Spacecrafts and Rockets 41 (2004)

3. Parsopoulos, K.E., Vrahatis, M.N.: Particle Swarm Optimization Method for Constrained Optimization Problems. University of Patras AI Research Center, GR-26110 Patras Greece

4. Akhtar, S., Linshu, H., Qazi, M.: Comparison of Pattern Search and Genetic Algorithm for Conceptual Design of Multi- Stage Liquid Rocket Missile. In: IFSA, pp. 1353–1359 (2005)

5. Venter, G., Sobieszczanski-Sobieski, J.: Multidisciplinary Optimization of a Transport Aircraft Wing using Particle Swarm Optimization. AIAA 2002–5644

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