DocumentCode
1794828
Title
Automatic landing on carrier method of unmanned air vehicle
Author
Lu Ke ; Wang Zhengzhong ; Yuan Suozhong
Author_Institution
Sci. & Technol. on Rotorcraft Aeromechanics Lab., Jingdezhen, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
299
Lastpage
302
Abstract
Automated carrier landing of an Unmanned Air Vehicle is a complex process. To successfully complete the task of landing on carrier, firstly the guidance system should give UAV flight control system a proper landing trajectory, then the flight control system according to the instructions given by the guidance system of UAV make the UAV fly on the right track, finally realizing automatic landing on carrier. In this process the guidance system providing correct guidance signal is a key factor in the success of landing on carrier. Now most aircraft carriers have angled deck, so there are great differences to ground-based landing. In view of this situation, a guidance law is designed for UAV landing on carrier, and the simulation of guidance law is carried out. Because of the air flow disturbance behind of the carrier, the requirement of flight control system is robust, so, this paper introduces quantitative feedback robust control design method to design the flight controller, in order to guarantee the robustness of control system. The results show that the guidance law and flight control system designed in this paper could realize the UAV autonomous landing.
Keywords
aerospace simulation; aircraft landing guidance; autonomous aerial vehicles; control system synthesis; feedback; robust control; trajectory control; UAV flight control system; UAV landing; air flow disturbance; aircraft carriers; angled deck; automated carrier landing; carrier method; flight controller design; ground-based landing; guidance law simulation; guidance signal; guidance system; landing trajectory; quantitative feedback robust control design method; robustness; unmanned air vehicle; Aerospace control; Aircraft; Control systems; Design methodology; Educational institutions; Global Positioning System; Robustness;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007248
Filename
7007248
Link To Document