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2013 | OriginalPaper | Chapter

Numerical Trajectory Optimization for Airborne Wind Energy Systems Described by High Fidelity Aircraft Models

Authors : Greg Horn, Sébastien Gros, Moritz Diehl

Published in: Airborne Wind Energy

Publisher: Springer Berlin Heidelberg

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In order to study design tradeoffs in the development of an AWE system, it is useful to develop a code to optimize a trajectory for arbitrary objective function and constraints. We present a procedure for using direct collocation to optimize such a trajectory where a model is specified as a set of differential–algebraic equations. The six degree of freedom single-kite, pumping-mode AWE model developed in

Chap. 10

is summarized, and two typical periodic optimal control problems are formulated and solved: maximum power and number of cycles per retraction. Finally, a procedure for optimally transitioning between two fixed trajectories is presented.

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Metadata
Title
Numerical Trajectory Optimization for Airborne Wind Energy Systems Described by High Fidelity Aircraft Models
Authors
Greg Horn
Sébastien Gros
Moritz Diehl
Copyright Year
2013
Publisher
Springer Berlin Heidelberg
DOI
https://doi.org/10.1007/978-3-642-39965-7_11