Improvement of quadrotor performance with flight control system using particle swarm proportional-integral-derivative (PS-PID)

The rapid development of microprocessor, electrical, sensors and advanced control technology make a quadrotor fast expansion. Unfortunately, a quadrotor is unstable and impossible to fly in fully open loop system. PID controller is one of methodology that has been proposed to control the flight cont...

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Bibliographic Details
Main Authors: Adriansyah, A. (Author), Amin, S. H. M. (Author), Minarso, A. (Author), Ihsanto, E. (Author)
Format: Article
Language:English
Published: Penerbit UTM Press, 2017.
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