Rapid Robust Design of a Deployable System for Boost-Glide Vehicles-Reference-Cited by-同舟云学术

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Rapid Robust Design of a Deployable System for Boost-Glide Vehicles

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Steinfeldt Bradley¹,Rossman Grant¹,Braun Robert¹,Barton Gregg²

Affiliation:

1. Georgia Institute of Technology

2. Draper Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-31

Reference35 articles.

1. 4Dwyer-Cianciolo, A. M., Davis, J. L., Komar, D. R., Munk, M. M., Samareh, J. A., Powell, R. W., Shidner, J. D., Stanley, D. O., Wilhite, A. W., Kinney, D. J., McGuire, M. K., Arnold, J. O., Howard, A. R., Sostaric, R. R., Studak, J. W., Zumwalt, C. H., Llama, E. G., Casoliva, J., Ivanov, M. C., Clark, I., and Sengupta, A. “Entry, Descent and Landing Systems Analysis Study: Phase 1 Report,” Tech. Rep. TM-2010-216720, NASA, July 2010.

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1. Extensibility of a linear rapid robust design methodology;Engineering Optimization;2015-06-26

2. Using Dynamical Systems Concepts in Multidisciplinary Design;AIAA Journal;2014-06

3. Extensibility of a Linear Rapid Robust Design Methodology;10th AIAA Multidisciplinary Design Optimization Conference;2014-01-10

4. Using Estimation Techniques in Multidisciplinary Design;10th AIAA Multidisciplinary Design Optimization Conference;2014-01-10

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