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...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Penerbit UTM Press
2017
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| Subjects: | |
| Online Access: | http://eprints.utm.my/76694/1/ShamsudinAmin2017_ImprovementofQuadrotorPerformancewithFlightControl.pdf |