PID Control Design of a Two-Degree-of-Freedom Helicopter Based on Differential Evolution and its Experimental Verification-Reference-Cited by-同舟云学术

PID Control Design of a Two-Degree-of-Freedom Helicopter Based on Differential Evolution and its Experimental Verification

Published:2017 Issue:11 Volume:30 Page:411-419
ISSN:1342-5668
Container-title:Transactions of the Institute of Systems, Control and Information Engineers
language:en
Short-container-title:Transactions of ISCIE

Author:

Yoshikawa Yuma¹,Kawata Masakatsu²

Affiliation:

1. Graduate School of System Informatics, Kobe University

2. Department of Control Engineering, National Institute of Technology,Maizuru College

Publisher

The Institute of Systems, Control and Information Engineers

Link

https://www.jstage.jst.go.jp/article/iscie/30/11/30_411/_pdf

Reference9 articles.

1. [1] J. Kennedy and R. Eberhart: Particle swarm optimization; Proceedings of IEEE International Conference on Neural Networks, pp. 1942-1948 (1995)

2. [2] R. Storn and K. Price: Differential evolution - a simple and efficient heuristic for global optimization over continuous spaces; Journal of Global Optimization, Vol. 11, pp. 341-359 (1997)

3. [6] Y. Minami and T. Muromaki: Differential evolution algorithm based design of discrete-valued input systems; Proceedings of SICE Annual Conference 2014, pp.333-336 (2014)

4. [7] M. S. Saad, H. Jamaluddin and I. Z. M. Darus: PID controller tuning using evolutionary algorithms;Wseas Transactions on Systems & Control, Vol. 7, No. 4, pp. 139-149 (2012)

5. [8] M. I. Solihin, R. Akmeliawati, R. Muhida and A. Legowo: Guaranteed robust state feedback controller via constrained optimization using differential evolution; Proceedings of the 6th International Colloquium on Signal Processing & Its Applications, pp. 272-277 (2010)