PID CONTROL OF A THREE-DEGREES-OF-FREEDOM MODEL HELICOPTER
| Main Author: | Aria, Muhammad |
|---|---|
| Format: | Article PeerReviewed |
| Bahasa: | eng |
| Terbitan: |
Lembaga Penelitian dan Pengabdian Masyarakat (LPPM) UNIKOM
, 2011
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| Subjects: | |
| Online Access: |
http://repository.unikom.ac.id/30545/1/10-miu-aria.pdf http://repository.unikom.ac.id/30545/ http://jurnal.unikom.ac.id/jurnal/pid-control-of-a.2g |
Daftar Isi:
- 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.