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Feedback Controller Design for Precision Turning of the Lockheed L1011 Tristar Aircraft

Hridi Juberi, Md. Tanvir Ahmed

Abstract


To have precise turning in an airplane simultaneous control over the rudder command and aileron command are the most significant as well as challenging parameters due to the possibility of imperfection coordinated turn. In response to the associated challenges in the turning of the aircraft, a state feedback controller has been designed to efficiently achieve the desired coordinated turn by controlling the input parameters (Rudder command, Aileron command) in terms of the associated states of the system. In this study, the designed controller perfectly achieves the stability and controllability of the input parameters by accurately coordinated turns through the systems' steady-state response. Hence, the findings of this study can facilitate the turning of aircraft by controlling the input parameters along with the states.


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References


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