Experimental H-infinity robust control of aerial vehicle flight

This paper proposes and evaluates the comparative studies between the classical controllers (PI, PD and PID) with H ∞ robust control technique for an 3-DOF helicopter. The control algorithm uses a robust controllers synthesized by the H ∞ loop shaping approach. The experimental results show that the...

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Published in2011 19th Mediterranean Conference on Control and Automation pp. 242 - 247
Main Authors Boukhnifer, Moussa, Chaibet, Ahmed, Larouci, Cherif
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.06.2011
Subjects
Dynamics
Frequency control
H ∞ loop shaping
Helicopter
Helicopters
Mathematical model
PD control
Robust control
Robustness
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ISBN9781457701245
1457701243
DOI10.1109/MED.2011.5982999

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Abstract This paper proposes and evaluates the comparative studies between the classical controllers (PI, PD and PID) with H ∞ robust control technique for an 3-DOF helicopter. The control algorithm uses a robust controllers synthesized by the H ∞ loop shaping approach. The experimental results show that the robust controllers stabilize the system and reject the disturbances when the system is subjected to uncertainties of a norm lower than the maximum stability margin.
AbstractList This paper proposes and evaluates the comparative studies between the classical controllers (PI, PD and PID) with H ∞ robust control technique for an 3-DOF helicopter. The control algorithm uses a robust controllers synthesized by the H ∞ loop shaping approach. The experimental results show that the robust controllers stabilize the system and reject the disturbances when the system is subjected to uncertainties of a norm lower than the maximum stability margin.
Author Boukhnifer, Moussa
Chaibet, Ahmed
Larouci, Cherif
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  givenname: Cherif
  surname: Larouci
  fullname: Larouci, Cherif
  organization: ESTACA Ecole d'Ing., Lab. Commande et Syst., Levallois-Perret, France
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Snippet This paper proposes and evaluates the comparative studies between the classical controllers (PI, PD and PID) with H ∞ robust control technique for an 3-DOF...
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StartPage 242
SubjectTerms Dynamics
Frequency control
H ∞ loop shaping
Helicopter
Helicopters
Mathematical model
PD control
Robust control
Robustness
Title Experimental H-infinity robust control of aerial vehicle flight
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