Universiti Teknologi Malaysia Institutional Repository

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

Adriansyah, A. and Amin, S. H. M. and Minarso, A. and Ihsanto, E. (2017) Improvement of quadrotor performance with flight control system using particle swarm proportional-integral-derivative (PS-PID). Jurnal Teknologi, 79 (6). pp. 121-128. ISSN 0127-9696

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Abstract

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 control system. Unfortunately, adjustment of PID parameters for robust control performance is not easy and still problems. The paper proposed a flight controller system based on a PID controller. The PID parameters are tuned automatically using Particle Swarm Optimization (PSO). Objective of this method is to improve the flight control system performance. Several experiments have been performed. According to these experiments the proposed system able to generate optimal and reliable PID parameters for robust flight controller. The system also has 41.57 % improvement in settling time response.

Item Type:Article
Uncontrolled Keywords:Flight control system, Performance improvement
Subjects:T Technology > TK Electrical engineering. Electronics Nuclear engineering
Divisions:Electrical Engineering
ID Code:76694
Deposited By: Fazli Masari
Deposited On:31 May 2018 09:25
Last Modified:31 May 2018 09:25

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