@inproceedings{5cb0100e1c704e8699a99a919da5dc94,
title = "Optimizing fuel consumption and reducing thermal load for a hypersonic vehicle",
abstract = "The range cruise of a future hypersonic flight vehicle is considered. Applying realistic models for vehicle dynamics and unsteady heat transfer, trajectory optimization is used to construct solutions for minimizing fuel consumption and reducing thermal loads. Efficient numerical techniques are used to cope with the difficulties of this complex optimal control problem.",
author = "M. W{\"a}chter and Tan, {R. C.E.} and G. Sachs and {Da Costa}, O.",
year = "2005",
language = "English",
isbn = "1563477297",
series = "A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "666--672",
booktitle = "A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference",
note = "13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference ; Conference date: 16-05-2005 Through 20-05-2005",
}