Design and implementation of 3-DOF helicopter bench test system
| dc.contributor.author | Sayeh Meddour, Yasser | |
| dc.contributor.author | Belghait, Naim | |
| dc.contributor.author | Ouadi, A. (Supervisor) | |
| dc.date.accessioned | 2022-06-15T12:06:34Z | |
| dc.date.available | 2022-06-15T12:06:34Z | |
| dc.date.issued | 2019 | |
| dc.description | 44 p. | en_US |
| dc.description.abstract | The scope of this project is to control the speed and the direction of dc motor using H-bridge and PWM and developing a mathematical model for the motor. It is asked to develop a 3-DOF (3 Degree Of Freedom) helicopter for laboratory experiment which is often used in control research education and analysis for the design and implementation of linear and non-linear control concepts. It is composed by three rotational joints, with the end bar carrying a pair of propellers actuated by DC motors. Measurements of the joints angles are supplied by incremental encoders. Two speed controllers based on Hbridges drivers for actuating the DC motor/propeller assemblies. Both angular measurements and control voltages provided by PC based hardware interfaces and software LABVIEW programs. Based on the identified model, a PID controller has been developed to control the speed of the motor. The simulation results show that the designed control system can guarantee high precision altitude and a good control under multi operation points | en_US |
| dc.description.sponsorship | Université M’Hamed BOUGARA de Boumerdes : Institut de génie electrique et electronique | en_US |
| dc.identifier.uri | https://dspace.univ-boumerdes.dz/handle/123456789/9458 | |
| dc.language.iso | en | en_US |
| dc.subject | PID controller | en_US |
| dc.subject | Labview | en_US |
| dc.subject | 3-DOF helicopter | en_US |
| dc.subject | PWM | en_US |
| dc.title | Design and implementation of 3-DOF helicopter bench test system | en_US |
| dc.type | Thesis | en_US |