WANG Jing, LIU Qiang. UAV Carrier Landing System Based on Backstepping[J]. Journal of nanchang hangkong university(Natural science edition), 2014, 28(3): 29-37. DOI: 10.3969/j.issn.1001-4926.2014.03.006
Citation: WANG Jing, LIU Qiang. UAV Carrier Landing System Based on Backstepping[J]. Journal of nanchang hangkong university(Natural science edition), 2014, 28(3): 29-37. DOI: 10.3969/j.issn.1001-4926.2014.03.006

UAV Carrier Landing System Based on Backstepping

  • This paper focus on the problem of UAV carrier landing. Through the use of UAV longitudinal dynamic model for validation platform, the validity of Backstepping control method is verified for UAV carrier landing system. In order to restraint the effect of wind and improve the precision of carrier landing, UAV carrier landing system is designed based on Backstepping. The automatic landing system was simulated, and the result showed that the requirement of carrier landing, restraint wind and excellent robustness were all achieved the performance specifications of the design. This control method can be widely applied in UAV carrier landing.
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