PID CONTROL OF A THREE-DEGREES-OF-FREEDOM MODEL HELICOPTER

Aria, Muhammad (2011) PID CONTROL OF A THREE-DEGREES-OF-FREEDOM MODEL HELICOPTER. Majalah Ilmiah UNIKOM, Volume. ISSN 1411-9374

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Abstract

Helicopter dynamic are in general nonlinear, time-varying and may be highly uncertain. This paper presents the design and implementation of a Proportional-Integral-Derivative (PID) Controller to control the elevation and travel of three-degrees-of freedom (3DOF) Helicopter. The controller is linear time-invariant and can be realized easily. The simulation results show that the designed control system can guarantee high precision altitude and elevation control under multi-operation points.

Item Type: Article
Uncontrolled Keywords: attitude control, 3dof, pid, helicopter dynamic, mimo systems
Subjects: Jurnal Tercetak > Majalah Ilmiah UNIKOM
Divisions: Universitas Komputer Indonesia > Direktorat > Lembaga Penelitian dan Pengabdian Masyarakat
Depositing User: M.Kom Taryana Suryana
Date Deposited: 30 Nov 2016 09:36
Last Modified: 30 Nov 2016 09:36
URI: https://repository.unikom.ac.id/id/eprint/30545

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