Multi-Phase Trajectory Optimization Methods with Applications to Hypersonic Vehicles-Reference-Cited by-同舟云学术

Multi-Phase Trajectory Optimization Methods with Applications to Hypersonic Vehicles

Published:1994 Issue: Volume: Page:133-164
ISSN:
Container-title:Applied Mathematics in Aerospace Science and Engineering
language:
Short-container-title:

Author:

Jänsch C.,Schnepper K.,Well K. H.

Publisher

Springer US

Link

http://link.springer.com/content/pdf/10.1007/978-1-4757-9259-1_8

Reference18 articles.

1. Schöttle, U. M., Flug-und Antriebsoptimierung luftatmender aerodynamischer Raumfahrtträger, Dissertation, University of Stuttgart, 1988 (in German).

2. Landiech, P., Aumasson, C., and Drox, Y., Airbreathing Launchers Trajectory Optimization, Preprint, 40th IAF Congress, Malaga, Spain, 1989.

3. Jänsch, C., Schnepper, K., and Well, K. H., Trajectory Optimization of a Transatmospheric Vehicle, Proceedings of the American Control Conference, Boston, Massachusetts, pp. 2232–2237, 1991.

4. Jänsch, C., Schnepper, K., and Well, K. H., Ascent and Descent Trajectory Optimization for Ariane V/Hermes, Preprint, 75th Symposium of the AGARD Flight Mechanics Panel on Space Vehicle Flight Mechanics, Luxembourg City, Luxembourg, 1989.

5. Cliff, E., Schnepper, K., and Well, K. H., Performance Analysis of a Transatmospheric Vehicle, Paper AIAA-90–5257, 2nd AIAA Aerospace Plane Conference, Orlando, Florida, 1990.

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