@inproceedings{30a3a4a80f6840a7b51ad052d76cde67,
title = "Reentry trajectory optimization for preventing overheating of damaged thermal protection system",
abstract = "An approach is presented for reducing the heat load at a damaged area of the thermal protection system by an appropriate reentry trajectory control and by temporarily commanding a sideslip angle. The purpose of commanding a sideslip angle is to generate an asymmetrical flow condition such that there is a shading affect of the body with regard to the damaged area. Using additionally an acceptable adaptation of path constraints for emergency cases, trajectory optimization is a means for coping with the safety problem of such a hazard scenario.",
author = "{Da Costa}, O. and G. Sachs",
year = "2005",
doi = "10.2514/6.2005-3272",
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 = "657--665",
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",
}