Modelling and PSO fine-tuned PID control of quadrotor UAV
This paper describes nonlinear dynamics model of x-configuration quadrotor using Newton-Euler modelling technique. To stabilize quadrotor attitude (roll (φ), pitch (θ), yaw (ψ)) during hovering, a PID controller is proposed. There is individual PID controller for each roll, pitch, yaw and z where 12...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Insight Society,
2017.
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| Subjects: | |
| Online Access: | Get fulltext |