2018 European Control Conference (ECC) 2018
DOI: 10.23919/ecc.2018.8550383
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Optimal Control of a Rigid-Wing Rotary Kite System for Airborne Wind Energy

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Cited by 10 publications
(10 citation statements)
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“…A periodic optimal control problem is formulated to maximize the average cycle power (P ) of a single AWES subject to equality and in-equality constraints described above (De Schutter et al, 2019;Leuthold et al, 2018). The trajectory optimization problem is discretized into 100 intervals using direct collocation.An initial guess is generated using a homotopy technique similar to (Gros et al, 2013) with an estimated circular trajectory based on a fixed number of loops (here n loop = 4) at a 30 • elevation angle and an estimated aircraft speed.…”
Section: Wind Boundary Conditionmentioning
confidence: 99%
“…A periodic optimal control problem is formulated to maximize the average cycle power (P ) of a single AWES subject to equality and in-equality constraints described above (De Schutter et al, 2019;Leuthold et al, 2018). The trajectory optimization problem is discretized into 100 intervals using direct collocation.An initial guess is generated using a homotopy technique similar to (Gros et al, 2013) with an estimated circular trajectory based on a fixed number of loops (here n loop = 4) at a 30 • elevation angle and an estimated aircraft speed.…”
Section: Wind Boundary Conditionmentioning
confidence: 99%
“…Although there exist many other interesting AWE concepts, e.g. those 31 based on tethered rotorcrafts [2,3], we will limit the scope of this paper to rigid-wing lift-32 Disclaimer/Publisher's Note: The statements, opinions, and data contained in all publications are solely those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). MDPI and/or the editor(s) disclaim responsibility for any injury to people or property resulting from any ideas, methods, instructions, or products referred to in the content.…”
Section: Introduction 22mentioning
confidence: 99%
“…transferred to the ground station through the tethers. Each aircraft k ∈ K generates 232 an amount of electrical power P turb,k := η turb κ k u a,k3 , with η turb the on-board turbine 233 efficiency. Note that for the case of power consumption, i.e.…”
mentioning
confidence: 99%
“…However, they are the standard in most AWES power estimation studies (e.g. [84,86,30,10]). AWES need to dy-namically adapt their flight trajectory to changing winds in order to optimize power production.…”
Section: Introductionmentioning
confidence: 99%