Flight path planning in a turbulent wind environment

Book Chapter (2018)
Author(s)

Uwe Fechner (TU Delft - Delft University Wind energy research institute)

Roland Schmehl (TU Delft - Wind Energy)

Research Group
Wind Energy
Copyright
© 2018 U. Fechner, R. Schmehl
DOI related publication
https://doi.org/10.1007/978-981-10-1947-0_15
More Info
expand_more
Publication Year
2018
Language
English
Copyright
© 2018 U. Fechner, R. Schmehl
Research Group
Wind Energy
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.@en
Pages (from-to)
361-390
ISBN (print)
9789811019463
ISBN (electronic)
978-981-10-1947-0
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

To achieve a high conversion efficiency and at the same time robust control of a pumping kite power system it is crucial to optimize the three-dimensional flight path of the tethered wing. This chapter extends a dynamic system model to account for a realistic, turbulent wind environment and adds a flight path planner using a sequence of attractor points and turn actions. Path coordinates are calculated with explicit geometric formulas. To optimize the power output the path is adapted to the average wind speed and the vertical wind profile, using a small set of parameters. The planner employs a finite state machine with switch conditions that are highly robust towards sensor errors. The results indicate, that the decline of the average power output of pumping kite power systems at high wind speeds can be mitigated. In addition it is shown, that reeling out towards the zenith after flying figure eight flight maneuvers significantly reduces the traction forces during reel-in and thus increases the total efficiency.

Files

Fechner_Schmehl2018_Chapter.pd... (pdf)
(pdf | 2.88 Mb)
- Embargo expired in 02-10-2018
License info not available