2016 American Control Conference (ACC) 2016
DOI: 10.1109/acc.2016.7525566
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A nonlinear adaptive controller for airborne wind energy systems

Abstract: Abstract-A nonlinear adaptive path following controller for a kite based airborne wind energy system is presented. For a given desired geometric path, we provide necessary conditions for closed-loop convergence of the kite to a tube centered around the desired path. The proposed controller is adapts for the case of unknown wind vector and kite parameters. The effectiveness of the approach is demonstrated via numerical simulations for multiple desired shapes of the geometric path and for varying desired tether … Show more

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Cited by 4 publications
(3 citation statements)
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“…Different guidance strategies for dealing with time-varying uncertainties have been derived, e.g. in Ahbe, Wood, and Smith (2018), Diwale, Alessandretti, Lymperopoulos, and Jones (2016), . In Wood, Ahbe, et al ( 2017), Wood et al (2018) and Rontsis, Costello, Lymperopoulos, and Jones (2015), path following control approaches with compensation for actuation delay were introduced.…”
Section: Other Approaches For Path Control and Pumping Operationmentioning
confidence: 99%
“…Different guidance strategies for dealing with time-varying uncertainties have been derived, e.g. in Ahbe, Wood, and Smith (2018), Diwale, Alessandretti, Lymperopoulos, and Jones (2016), . In Wood, Ahbe, et al ( 2017), Wood et al (2018) and Rontsis, Costello, Lymperopoulos, and Jones (2015), path following control approaches with compensation for actuation delay were introduced.…”
Section: Other Approaches For Path Control and Pumping Operationmentioning
confidence: 99%
“…The control signal u γ is the rate of change of the heading angle. A more detailed description of the kite mathematical model can be found in the work of Diwale et al The kite kinematics is given by the following system of ODEs: rightL00Lcosfalse(θfalse)trueθ̇trueϕ̇left=R¯NK10E000RNKTRGNTvwR¯NKEz0rightrightγ̇left=uγ, where trueR¯NK, R NK , and R GN are the following rotation matrices: rightRGNleft=sinθcosϕsinϕcosθcosϕsinθsinϕcosϕcosθsinϕcosθ0sinθ,RNK=trueR¯NKbold0bold0…”
Section: Implementation Examplesmentioning
confidence: 99%
“…The control signal u is the rate of change of the heading angle. A more detailed description of the kite mathematical model can be found in the work of Diwale et al 21 The kite kinematics is given by the following system of ODEs:…”
Section: Example 1: Model Predictive Path Following Controller For Pomentioning
confidence: 99%