Fundamental Control System Design Issues for Scramjet-Powered Hypersonic Vehicles-Reference-Cited by-同舟云学术

Fundamental Control System Design Issues for Scramjet-Powered Hypersonic Vehicles

Published:2015-01-02 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Echols Justin A.¹,Puttannaiah Karan¹,Mondal Kaustav¹,Rodriguez Armando¹

Affiliation:

1. Arizona State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1760

Reference74 articles.

1. The X-43A Six Degree of Freedom Monte Carlo Analysis

2. X-43 - Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006

3. 4V. L. Rausch, C. R. McClinton, and J. L. Crawford, "Hyper-X Flight Validation of Hypersonic Airbreathing Technology," Technical Report, NASA Hyper-X Program Office, pp.1 - 7, 1997.

4. YALMIP : a toolbox for modeling and optimization in MATLAB

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