Research Article

CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL

Volume: 4 Number: 3 September 28, 2017
EN

CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL

Abstract

The paper introduces different control design methods for nonlinear systems with their application to the nonlinear mathematical model of a 3 DOF helicopter. Recent studies on the control design approaches, such as State Dependent Riccati Equation based optimal controller, Model Reference Adaptive Control and Sliding Mode Control, are reviewed and design methodologies are given. Then the mathematical model of a 3 DOF helicopter dynamics is derived and simplified with the software called CIFER. By using the simplified mathematical model of the 3 DOF helicopter, the control algorithms are applied to the model in order to explore the performances of the controllers. The results are given in the simulation environment. The paper is presented in a tutorial manner in order to explain the applications of the proposed nonlinear control methodologies.

Keywords

References

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  3. [3] Zhai, Y., Nounou, M., Nounou, H. and Al-Hamidi, Y., "Model Predictive Control of a 3-DOF Helicopter System Using Successive Linearization", International Journal of Engineering, Science and Technology, 2(10): 9-19, (2010).
  4. [4] Liu, Z., el haj, Z. C. and Shi, H., "Control Strategy Design Based on Fuzzy Logic and LQR for 3-DOF Helicopter Model", International Conference on Intelligent Control and Information Processing, Dalian, (2010).
  5. [5] Zhang, J., Cheng, X. and Zhu, J., "Control of a Laboratory 3-DOF Helicopter: Explicit Model Predictive Approach", International Journal of Control, Automation and Systems, 14(2): 389-399, (2016).
  6. [6] Nishi, M., Ishitobi, M. and Nakasaki, K., "Nonlinear Adaptive Control System Design and Experiment for a 3-DOF Model Helicopter", Artif Life Robotics, 13: 50-53, (2008).
  7. [7] Boby, R.I., Mansor, H., Gunawan, T.S. and Khan, S., "Robust Adaptive LQR Control of Nonlinear System Application to 3-Dof Flight Control System", IEEE International Conference on Smart Instrumentation, Measurement and Applications (ICSIMA), Kuala Lumpur, (2014).
  8. [8] Pearson, J.D., "Approximation Methods in Optimal Control", Journal of Electronics and Control, 13: 453-469, (1962).

Details

Primary Language

English

Subjects

-

Journal Section

Research Article

Authors

Bedrettin Mahmut Kocagil
Gazi University
Türkiye

Ahmet Çağrı Arıcan
Gazi University
Türkiye

Ümit Müfit Güzey This is me
Gazi University
Türkiye

Sinan Özcan This is me
Gazi University
Türkiye

Metin U. Salamci
Gazi University
Türkiye

Publication Date

September 28, 2017

Submission Date

July 18, 2017

Acceptance Date

September 22, 2017

Published in Issue

Year 2017 Volume: 4 Number: 3

APA
Kocagil, B. M., Arıcan, A. Ç., Güzey, Ü. M., Özcan, S., & Salamci, M. U. (2017). CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL. Gazi University Journal of Science Part A: Engineering and Innovation, 4(3), 47-66. https://izlik.org/JA97AE35GC
AMA
1.Kocagil BM, Arıcan AÇ, Güzey ÜM, Özcan S, Salamci MU. CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL. GU J Sci, Part A. 2017;4(3):47-66. https://izlik.org/JA97AE35GC
Chicago
Kocagil, Bedrettin Mahmut, Ahmet Çağrı Arıcan, Ümit Müfit Güzey, Sinan Özcan, and Metin U. Salamci. 2017. “CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL”. Gazi University Journal of Science Part A: Engineering and Innovation 4 (3): 47-66. https://izlik.org/JA97AE35GC.
EndNote
Kocagil BM, Arıcan AÇ, Güzey ÜM, Özcan S, Salamci MU (September 1, 2017) CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL. Gazi University Journal of Science Part A: Engineering and Innovation 4 3 47–66.
IEEE
[1]B. M. Kocagil, A. Ç. Arıcan, Ü. M. Güzey, S. Özcan, and M. U. Salamci, “CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL”, GU J Sci, Part A, vol. 4, no. 3, pp. 47–66, Sept. 2017, [Online]. Available: https://izlik.org/JA97AE35GC
ISNAD
Kocagil, Bedrettin Mahmut - Arıcan, Ahmet Çağrı - Güzey, Ümit Müfit - Özcan, Sinan - Salamci, Metin U. “CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL”. Gazi University Journal of Science Part A: Engineering and Innovation 4/3 (September 1, 2017): 47-66. https://izlik.org/JA97AE35GC.
JAMA
1.Kocagil BM, Arıcan AÇ, Güzey ÜM, Özcan S, Salamci MU. CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL. GU J Sci, Part A. 2017;4:47–66.
MLA
Kocagil, Bedrettin Mahmut, et al. “CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL”. Gazi University Journal of Science Part A: Engineering and Innovation, vol. 4, no. 3, Sept. 2017, pp. 47-66, https://izlik.org/JA97AE35GC.
Vancouver
1.Bedrettin Mahmut Kocagil, Ahmet Çağrı Arıcan, Ümit Müfit Güzey, Sinan Özcan, Metin U. Salamci. CONTROLLER DESIGNS FOR NONLINEAR SYSTEMS WITH APPLICATION TO 3 DOF HELICOPTER MODEL. GU J Sci, Part A [Internet]. 2017 Sep. 1;4(3):47-66. Available from: https://izlik.org/JA97AE35GC