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

DOI

10.2991/icmmcce-15.2015.441How to use a DOI?

Keywords

carrier air wake, inverse dynamic, PID control

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 combined 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.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hengzhi Ding
PY  - 2015/12
DA  - 2015/12
TI  - Design of Automatic Carrier Landing System Based on Dynamic Inverse and PID Control
BT  - Proceedings of the 4th International Conference on Mechatronics, Materials, Chemistry and Computer Engineering 2015
PB  - Atlantis Press
SP  - 1203
EP  - 1209
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmcce-15.2015.441
DO  - 10.2991/icmmcce-15.2015.441
ID  - Ding2015/12
ER  -