Simulation and experimental study on PID control of a quadrotor MAV with perturbation
This paper presents a proportional-integral-derivative (PID) flight controller for a quadrotor micro air vehicle (MAV). The MAV (Parrot Mambo minidrones) is small, therefore, a slight perturbation will affect its performance. Hence, for the actuated dynamics, roll (?), pitch (?), yaw (?), and z stab...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Institute of Advanced Engineering and Science
2020
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| Subjects: | |
| Online Access: | http://eprints.utm.my/93504/1/MohdAriffananMohdBasri2020_SimulationAndExperimentalStudyOnPIDControl.pdf |