TY - GEN
T1 - A direct solution approach for multi timescale optimal control problems
AU - Bittner, Matthias
AU - Grüter, Benedikt
AU - Diepolder, Johannes
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2017 International Center for Numerical Methods in Engineering. All rights reserved.
PY - 2017
Y1 - 2017
N2 - In high fidelity optimal control problems, a commonly appearing problem emerges from different timescales inherent to the model, resulting in stiff differential equations. When solving these problems using direct discretization, the selection of the discretization nodes for all States is driven by the States associated with the fast dynamics, no matter how strong their influence on the solution is. In this paper, a novel discretization scheme is presented that uses direct collocation for the slow States while the fast States of the model are represented based on a direct multiple shooting scheme. This way, different grids may be chosen for the States, resulting in a slight decoupling of the timescales. A high fidelity air race trajectory optimization problem is implemented to demonstrate how the dimensions of the discretized problem can be significantly decreased by the method, resulting in improved computational performance during the solution process.
AB - In high fidelity optimal control problems, a commonly appearing problem emerges from different timescales inherent to the model, resulting in stiff differential equations. When solving these problems using direct discretization, the selection of the discretization nodes for all States is driven by the States associated with the fast dynamics, no matter how strong their influence on the solution is. In this paper, a novel discretization scheme is presented that uses direct collocation for the slow States while the fast States of the model are represented based on a direct multiple shooting scheme. This way, different grids may be chosen for the States, resulting in a slight decoupling of the timescales. A high fidelity air race trajectory optimization problem is implemented to demonstrate how the dimensions of the discretized problem can be significantly decreased by the method, resulting in improved computational performance during the solution process.
KW - Aircraft trajectory optimization
KW - Direct discretization
KW - Multiple timescales
KW - Optimal control
KW - Stiff dynamics
UR - http://www.scopus.com/inward/record.url?scp=85045337597&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85045337597
T3 - Proceedings of the 7th International Conference on Coupled Problems in Science and Engineering, COUPLED PROBLEMS 2017
SP - 1121
EP - 1132
BT - Proceedings of the 7th International Conference on Coupled Problems in Science and Engineering, COUPLED PROBLEMS 2017
A2 - Papadrakakis, Manolis
A2 - Onate, Eugenio
A2 - Schrefler, Bernhard A.
PB - International Center for Numerical Methods in Engineering
T2 - 7th International Conference on Coupled Problems in Science and Engineering, COUPLED PROBLEMS 2017
Y2 - 12 June 2017 through 14 June 2017
ER -