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Design of Automatic Carrier Landing System Based on Dynamic Inverse and PID Control

Hengzhi Ding
2015 Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015   unpublished

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a Dshinji137@163.com. Abstract. At last twenty seconds of carrier landing process, the carrier-based aircraft will encounter with strong carrier air wake which will easily cause a deviation in the aircraft's path, at the same time, a carrier also has a six-degree-of-freedom motion which depends on carrier's property and sea state [6] . Without an efficient control in the aircraft, it will easily result a fatal crash. In this paper, the author use the theory of nonlinear inverse dynamics
more » ... with PID control to design an automatic carrier landing system which can efficiently resist carrier air wake and can limit lateral position error and vertical height error in 1m and longitudinal position error in 5m on sea state level 4 in the simulation of Simulink.
doi:10.2991/icmmcce-15.2015.441 fatcat:3xs7ec4t4bfcppygupt7hsr6ye
Citation

Hengzhi Ding. "Design of Automatic Carrier Landing System Based on Dynamic Inverse and PID Control." Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015 (2015)