Modeling of Closed Loop PID Controller for an Auto-Pilot Aircraft Roll Control
نویسنده
چکیده
---An aircraft contains three rotational motions like pitch, yaw and roll. The roll motion is controlled by the ailerons that are present on either side of an aircraft. In this paper, ailerons are considered as plant and its transfer function is used in modeling of the controller. The PID controller modeled performs better roll motion with good stability. From the MATLAB simulation results it is shown that the PID controller has the ability to minimize error between input and output with more stability and less response time with considerable
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