DESIGN OF INTEGRAL AUGMENTED SLIDING MODE CONTROL FOR PITCH ANGLE OF A 3-DOF BENCH-TOP HELICOPTER

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ZAERI A.H.; BAHARI MOHD NOOR S.; MOHD ISA M.; TAIP F.S.

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Journal Paper

Paper Information

Journal: Majlesi Journal of Electrical Engineering Year:2010 | Volume:4 | Issue:3 (14) Page(s): 31-35

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Title

DESIGN OF INTEGRAL AUGMENTED SLIDING MODE CONTROL FOR PITCH ANGLE OF A 3-DOF BENCH-TOP HELICOPTER

Author(s)

ZAERI A.H. | BAHARI MOHD NOOR S. | MOHD ISA M. | TAIP F.S. | Issue Writer Certificate

Keywords

SLIDING MODE CONTROL

CHATTERING PHENOMENON

BOUNDARY LAYER

PITCH ANGEL OF A 3-DOF HELICOPTER

Abstract

SLIDING MODE CONTROL (SMC) is a nonlinear controller that is used to achieve desired performance in the presence of unstructured uncertainty as a result of carelessness of parameter specification of the system. The main aim for sliding control, or also called Variable Structure Control, is to control the nonlinear plant by introducing a sliding surface. The sliding surface should be reached by making the state of system approach this level. In this paper, an integral augmented SLIDING MODE CONTROL (SMC+I) is proposed to improve the control performance of a plant with uncertainty giving the example of bench-top helicopter and the results are compared with the results obtained from conventional SLIDING MODE CONTROL with and without a BOUNDARY LAYER.

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APA: Copy

ZAERI, A.H., BAHARI MOHD NOOR, S., MOHD ISA, M., & TAIP, F.S.. (2010). DESIGN OF INTEGRAL AUGMENTED SLIDING MODE CONTROL FOR PITCH ANGLE OF A 3-DOF BENCH-TOP HELICOPTER. MAJLESI JOURNAL OF ELECTRICAL ENGINEERING, 4(3 (14)), 31-35. SID. https://sid.ir/paper/572650/en

Vancouver: Copy

ZAERI A.H., BAHARI MOHD NOOR S., MOHD ISA M., TAIP F.S.. DESIGN OF INTEGRAL AUGMENTED SLIDING MODE CONTROL FOR PITCH ANGLE OF A 3-DOF BENCH-TOP HELICOPTER. MAJLESI JOURNAL OF ELECTRICAL ENGINEERING[Internet]. 2010;4(3 (14)):31-35. Available from: https://sid.ir/paper/572650/en

IEEE: Copy

A.H. ZAERI, S. BAHARI MOHD NOOR, M. MOHD ISA, and F.S. TAIP, “DESIGN OF INTEGRAL AUGMENTED SLIDING MODE CONTROL FOR PITCH ANGLE OF A 3-DOF BENCH-TOP HELICOPTER,” MAJLESI JOURNAL OF ELECTRICAL ENGINEERING, vol. 4, no. 3 (14), pp. 31–35, 2010, [Online]. Available: https://sid.ir/paper/572650/en

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