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|Title:||Optimizing fuel consumption and reducing thermal load for a hypersonic vehicle||Authors:||Wächter, M.
Da Costa, O.
|Issue Date:||2005||Citation:||Wächter, M.,Tan, R.C.E.,Sachs, G.,Da Costa, O. (2005). Optimizing fuel consumption and reducing thermal load for a hypersonic vehicle. A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference 1 : 666-672. ScholarBank@NUS Repository.||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.||Source Title:||A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference||URI:||http://scholarbank.nus.edu.sg/handle/10635/104606||ISBN:||1563477297|
|Appears in Collections:||Staff Publications|
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