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

• Main Authors: Adriansyah, A., Amin, S. H. M., Minarso, A., Ihsanto, E.
• Format: Article
• Language: English
• Published: Penerbit UTM Press 2017
• Subjects: TK Electrical engineering. Electronics Nuclear engineering
• Online Access: http://eprints.utm.my/id/eprint/76694/1/ShamsudinAmin2017_ImprovementofQuadrotorPerformancewithFlightControl.pdf; http://eprints.utm.my/id/eprint/76694/; https://www.scopus.com/inward/record.uri?eid=2-s2.0-85028534275&doi=10.1111.%2fjt.v79.10680&partnerID=40&md5=492f6955374bd3e0c1a87b1d0dc9f4ce

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...