Title :
An autonomous carrier landing system design and simulation for unmanned aerial vehicle
Author :
Lu Keke ; Li Qing ; Cheng Nong
Author_Institution :
Navig., Guidance & Control Lab., Tsinghua Univ., Beijing, China
Abstract :
This paper focuses on the key issues of landing a carrier-based fixed-wing UAV on the aircraft carrier, especially the autonomous landing system design principles, methods and simulation. According to the differences between piloted and unmanned landing, including the distinction of landing on the land and moving carrier, this paper proposes autonomous landing system design issues and requirements. Adaptive deck motion prediction and compensation is used, with appropriate wave-off decision-making method, while an integrated design of the flight control system and automatic thrust control system is used to follow the glide slope precisely. Finally, based on the designs, an autonomous aircraft carrier landing system is completed and simulated with desired performance.
Keywords :
aerospace control; aerospace simulation; aircraft landing guidance; autonomous aerial vehicles; control system synthesis; decision making; mobile robots; motion compensation; adaptive deck motion compensation; adaptive deck motion prediction; automatic thrust control system design; autonomous aircraft carrier landing system; autonomous carrier landing system design; autonomous carrier landing system simulation; carrier-based fixed-wing UAV landing; flight control system design; unmanned aerial vehicle; wave-off decision-making method; Aerospace control; Aircraft; Atmospheric modeling; Control systems; Marine vehicles; Radar tracking;
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
DOI :
10.1109/CGNCC.2014.7007393