Multidisciplinary Design Optimization of Multi-Stage Launch Vehicle using Flight Phases Decomposition-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization of Multi-Stage Launch Vehicle using Flight Phases Decomposition

Published:2010-07 Issue:3-4 Volume:4 Page:117-125
ISSN:1779-627X
Container-title:International Journal for Simulation and Multidisciplinary Design Optimization
language:
Short-container-title:Int. J. Simul. Multidisci. Des. Optim.

Author:

Balesdent Mathieu,Bérend Nicolas,Dépincé Philippe,Chriette Abdelhamid

Publisher

EDP Sciences

Subject

Control and Optimization,Modelling and Simulation

Link

http://www.ijsmdo.org/10.1051/ijsmdo/2010015/pdf

Reference9 articles.

1. Design Optimization of a Space Launch Vehicle Using a Genetic Algorithm

2. R. Braun and I. Kroo,Development and application of the Collaborative Optimization architecture in a multidisciplinary design environment : State of the Art, SIAM, 98-116, (1996).

3. N. Duranté, A. Dufour, V. Pain,Multidisciplinary Analysis and Optimisation Approach for the Design of Expendable Launchers, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, New-York, USA (2004).

4. ESA Directorate of launchers,ESA Launch Vehicle Catalogue, (2004).

5. R.W. Humble, G.N. Henry, W.J. Larson,Space propulsion analysis and design, The McGraw-Hill Companies, Inc. (1995).

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