Aria, Muhammad (2011) PID CONTROL OF A THREE-DEGREES-OF-FREEDOM MODEL HELICOPTER. Majalah Ilmiah UNIKOM, Volume. ISSN 1411-9374
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Official URL: http://jurnal.unikom.ac.id/jurnal/pid-control-of-a...
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 |
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| 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: | Admin Repository |
| Date Deposited: | 30 Nov 2016 09:36 |
| Last Modified: | 30 Nov 2016 09:36 |
| URI: | http://repository.unikom.ac.id/id/eprint/30545 |
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