Hybrid intelligent control of a lab model helicopter pitch dynamics

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

In this paper, the pitch angle control for a lab model helicopter is discussed. This problem has some specific features. As a main unusual feature, it is observed that the steady state control command is completely dependent on the setpoint, so error-based controllers do not suit this problem. Moreover, the system is of a highly oscillating dynamic. In order to solve this control problem, two controllers are designed, an artificial neural network, whose input is the setpoint, is used to provide steady state control command, and a fuzzy inference system ,whose input is error, is used to provide transient control command. The total control command is the sum of two aforementioned control commands. The system's robustness is also checked against any probable disturbance and parameter change. It is shown that the system is likely to be completely robust against any possible disturbance or parameter change in lab environment. In order make the system robust against a special kind of parameter change which is impossible to happen in the lab, a setpoint modification algorithm is offered to vanish the steady state error and provide a rather short settling time.

Original languageEnglish
Title of host publication2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007
Pages162-166
Number of pages5
DOIs
Publication statusPublished - 2007
Event2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007 - Kuala Lumpur, Malaysia
Duration: Nov 25 2007Nov 28 2007

Other

Other2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007
CountryMalaysia
CityKuala Lumpur
Period11/25/0711/28/07

Fingerprint

Intelligent control
Helicopters
Controllers
Fuzzy inference
Neural networks

ASJC Scopus subject areas

  • Artificial Intelligence
  • Control and Systems Engineering

Cite this

Mohammadzaheri, M., & Chen, L. (2007). Hybrid intelligent control of a lab model helicopter pitch dynamics. In 2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007 (pp. 162-166). [4658367] https://doi.org/10.1109/ICIAS.2007.4658367

Hybrid intelligent control of a lab model helicopter pitch dynamics. / Mohammadzaheri, Morteza; Chen, Ley.

2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007. 2007. p. 162-166 4658367.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Mohammadzaheri, M & Chen, L 2007, Hybrid intelligent control of a lab model helicopter pitch dynamics. in 2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007., 4658367, pp. 162-166, 2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007, Kuala Lumpur, Malaysia, 11/25/07. https://doi.org/10.1109/ICIAS.2007.4658367
Mohammadzaheri M, Chen L. Hybrid intelligent control of a lab model helicopter pitch dynamics. In 2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007. 2007. p. 162-166. 4658367 https://doi.org/10.1109/ICIAS.2007.4658367
Mohammadzaheri, Morteza ; Chen, Ley. / Hybrid intelligent control of a lab model helicopter pitch dynamics. 2007 International Conference on Intelligent and Advanced Systems, ICIAS 2007. 2007. pp. 162-166
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