Application of intelligent controller in feedback control loop for aircraft pitch control

• Main Authors: Wahid, N., Hassan, N., Rahmat, M. F., Mansor, S.
• Format: Article
• Published: INSInet Publications 2011
• Subjects: TJ Mechanical engineering and machinery
• Online Access: http://eprints.utm.my/id/eprint/44746/

This paper presents the investigation into the development of hybrid control scheme for pitch control of aircraft system. Proportional-integral-derivative (PID) and PID-type fuzzy logic controller are used in this investigation to control the pitch angle of aircraft system. The dynamic modeling of s...