Application of intelligent controller in feedback control loop for aircraft pitch control
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...
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Main Authors: | , , , |
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Format: | Article |
Published: |
INSInet Publications
2011
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Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/44746/ |
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Institution: | Universiti Teknologi Malaysia |