Title :
Kinetic simulation research on the aircraft landing and arresting
Author :
Zhang Zhi ; Zou Sheng-tao ; Zhu Qi-dan
Author_Institution :
Coll. of Autom., Harbin Eng. Univ., Harbin, China
Abstract :
The danger of Aircraft carrier was in the stage of landing and arrested, which mainly due to the vertical and horizontal speed. To summarize some of the droping block law, in this paper, a certain type of aircraft is studied, the dynamic modeling of the motion process of the airframe, landing gear, tail hook and blocking force is created, then create simulation system including the process of “landing gear droping”, “tail hook bouncing”and“aircraft arrested”, then the corresponding law of motion is obtained by setting different blocking conditions, which can provide a reference for the protection of the safety of the aircraft when landing and arrested.
Keywords :
aircraft landing guidance; vehicle dynamics; aircraft arresting; aircraft carrier; aircraft landing; aircraft safety protection; airframe dynamic modeling; airframe motion process; blocking force; droping block law; horizontal speed; kinetic simulation research; landing gear; landing gear droping; law of motion; tail hook; tail hook bouncing; vertical speed; Aircraft; Aircraft propulsion; Atmospheric modeling; Dynamics; Educational institutions; Electronic mail; Gears; aircraft; dynamic modeling; law of motion; simulation system;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896001
