Instationary Heat-Constrained Trajectory Optimization of a Hypersonic Space Vehicle by ODE–PDE-Constrained Optimal Control

DOI10.1007/978-0-387-95857-6_8zbMath1185.76864OpenAlexW2125865038MaRDI QIDQ3407685

Gottfried Sachs, Florent le Bras, Kurt Chudej, Markus Wächter, Hans Josef Pesch

Publication date: 4 March 2010

Published in: Variational Analysis and Aerospace Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-0-387-95857-6_8

Mathematics Subject Classification ID

Finite difference methods for boundary value problems involving PDEs (65N06) Flow control and optimization for compressible fluids and gas dynamics (76N25)

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Cites Work

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• Reduction of coolant fuel losses in hypersonic flight by optimal trajectory control
• Modelling of Heat Transfer and Vehicle Dynamics for Thermal Load Reduction by Hypersonic Flight Optimization
• A Differentiation Index for Partial Differential-Algebraic Equations
• Simulation of convective heat flux and heat penetration for a spacecraft at re-entry
• Minimizing the maximum heating of a re-entering space shuttle: An optimal control problem with multiple control constraints

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