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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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Penerbit UTM Press
2017
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| 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 |
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http://eprints.utm.my/id/eprint/76694/1/ShamsudinAmin2017_ImprovementofQuadrotorPerformancewithFlightControl.pdfhttp://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