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...

Full description

Saved in:
Bibliographic Details
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
Online AccessGet full text
ISBN9781457701245
1457701243
DOI10.1109/MED.2011.5982999

Cover

More Information
Summary: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.
ISBN:9781457701245
1457701243
DOI:10.1109/MED.2011.5982999