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

fYear

2014

fDate

28-30 July 2014

Firstpage

6174

Lastpage

6179

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2014 33rd Chinese

Conference_Location

Nanjing

Type

conf

DOI

10.1109/ChiCC.2014.6896001

Filename

6896001