@article{MAKHILLJEAS202116319523,
    title = {Flight Control System Based On PID Controller for Pitch of Aircraft B747},
    journal = {Journal of Engineering and Applied Sciences},
    volume = {16},
    number = {3},
    pages = {119-125},
    year = {2021},
    issn = {1816-949x},
    doi = {jeasci.2021.119.125},
    url = {https://makhillpublications.co/view-article.php?issn=1816-949x&doi=jeasci.2021.119.125},
    author = {C.},
    keywords = {PID controller,pitch control,longitudinal dynamic,autopilot},
    abstract = {Today’s aircraft designs rely heavily on
automatic control system to monitor and control many of
aircraft’s subsystem. The development of this work is to
model a pitch controller based an autopilot that controls
the pitch of an aircraft. The PID controller and model
predictive controller are developed for controlling the
pitch angle of an aircraft system. Simulation results for
the response of pitch controller are presented in short
period aircraft. Finally, the performances of pitch control
systems are investigated and analyzed based on common
criteria of step’s response. PID controller give the best
performance, it was optimal.}
    }