2 May 2006 The analysis on nonlinear control of the aircraft arresting system
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Proceedings Volume 6042, ICMIT 2005: Control Systems and Robotics; 60420K (2006) https://doi.org/10.1117/12.664551
Event: ICMIT 2005: Merchatronics, MEMS, and Smart Materials, 2005, Chongqing, China
The aircraft arresting system is a complicated nonlinear system. This paper analyzes the mechanical-hydraulic structure of aircraft arresting system composed of electro hydraulic valve and establishes the dynamic equation of the aircraft arresting system. Based on the state-feedback linearization of nonlinear system, a PD-based controller is synthesized. Simulation studies indicate, while arresting the different type aircraft, the proposed controller has fast response, good tracking performance and strong robustness. By tuning the parameters of the PD controller, a satisfactory control performance can be guaranteed.
© (2006) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jinchun Song, Jinchun Song, Tianrong Du, Tianrong Du, } "The analysis on nonlinear control of the aircraft arresting system", Proc. SPIE 6042, ICMIT 2005: Control Systems and Robotics, 60420K (2 May 2006); doi: 10.1117/12.664551; https://doi.org/10.1117/12.664551

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