DocumentCode :
2988257
Title :
Kinematics Analysis and Simulation on Formation-Based Space Net Dragging Process
Author :
Zhijie Gao ; Dongfang Yang ; Haibo Min ; Fuchun Sun
Author_Institution :
Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing, China
fYear :
2012
fDate :
7-9 Dec. 2012
Firstpage :
455
Lastpage :
460
Abstract :
Formation-based space net capture is a novel mode for spacecraft capturing and docking. After the object is successfully captured by space net, the relative movement model is firstly established based on the orbit elements after the target has been captured. Then, main disturbance elements for the spacecraft in the process of space net dragging are analyzed in detail. Besides, numerical simulations are carried out, whose results show that the formation mode is an effective means for investigating the complex compounded body movement. Moreover, the movement law between spacecraft and its capture target is derived via simulation. It turns out that the target will surround the spacecraft around its orbit.
Keywords :
aerospace control; celestial mechanics; kinematics; motion control; numerical analysis; position control; space vehicles; body movement; formation mode; formation-based space net capture; formation-based space net dragging process; kinematics analysis; movement law; numerical simulation; object capture; orbit element; relative movement model; spacecraft capturing; spacecraft docking; Earth; Kinematics; Mathematical model; Orbits; Satellites; Simulation; Space vehicles; disturbance; dragging process; formation; orbital elements; space net;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Engineering and Communication Technology (ICCECT), 2012 International Conference on
Conference_Location :
Liaoning
Print_ISBN :
978-1-4673-4499-9
Type :
conf
DOI :
10.1109/ICCECT.2012.119
Filename :
6414065
Link To Document :
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