Cessna-172P Autopilot Wing Leveler Ziegler-Nichols PID Control Method
ZHAO Xinye
LIANG Haiming
SUN Guangming
YANG Fan
Abstract：In order to solve the chosen problem of Cessna-172P autopilot wing leveler PID control parameters,Ziegler-Nich?ols method is proposed. Ziegler-Nichols PID controller the adaptive PID controller doesn't need any prior knowledge of the process and build any process model,and can keep the control loop operating efficiently. The method can control Cessna-172P autopilot wing leveler adaptively,which is implemented in JSBSim flight simulation system. Simulation experiments display the controller has a better dynamic respond performance in overall situation.
Keywords：autopilotwing levelerZiegler-NicholsPID ControlJSBSim
Publication Date：2017-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：5( 1081-1085 )