Improved Twin Rotor mimo System tracking and transient response using Fuzzy control technology

Chuan Sheng Liu, Liang-Rui Chen, Chen Sheng Ting, Jonq Chin Hwang, Shing Lih Wu

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

This work obtains the appropriate parameters for proportional, integral, and derivative controllers for a Twin Rotor Multivariable System to achieve good tracking performance using a novel method combined with the model reduction method. The Fuzzy control method with the multi-section gains and derivatives is also applied to improve tracking performance and solve the disturbance problem caused by the air flows. Both methods are implemented by the proposed real-time control system. Simulation and experiment results verify the effectiveness of the proposed methods.

Original languageEnglish
Pages (from-to)37-43
Number of pages7
JournalJournal of Aeronautics, Astronautics and Aviation
Volume43
Issue number1
Publication statusPublished - 2011 Jan 1

Fingerprint

transient response
Fuzzy control
Transient analysis
rotors
Rotors
Derivatives
Multivariable systems
Real time control
air flow
controllers
disturbances
Control systems
Controllers
Air
simulation
Experiments
airflow
control system
method
disturbance

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Liu, Chuan Sheng ; Chen, Liang-Rui ; Ting, Chen Sheng ; Hwang, Jonq Chin ; Wu, Shing Lih. / Improved Twin Rotor mimo System tracking and transient response using Fuzzy control technology. In: Journal of Aeronautics, Astronautics and Aviation. 2011 ; Vol. 43, No. 1. pp. 37-43.
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Improved Twin Rotor mimo System tracking and transient response using Fuzzy control technology. / Liu, Chuan Sheng; Chen, Liang-Rui; Ting, Chen Sheng; Hwang, Jonq Chin; Wu, Shing Lih.

In: Journal of Aeronautics, Astronautics and Aviation, Vol. 43, No. 1, 01.01.2011, p. 37-43.

Research output: Contribution to journalArticle

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