DocumentCode
2446867
Title
Control system design and simulation of spacecraft formations
Author
Reyhanoglu, Mahmut ; Dyer, Daniel
Author_Institution
Phys. Sci. Dept., Embry-Riddle Aeronaut. Univ., Daytona Beach, FL
fYear
2008
fDate
10-13 Nov. 2008
Firstpage
120
Lastpage
125
Abstract
This paper presents an effective control scheme for spacecraft formations. Modifying earlier established control design techniques, feedback laws are constructed to control translational and rotational motion of a group of spacecraft. Computer simulations are carried out to illustrate the effectiveness of the control laws. The ephemeris and attitude data generated through the simulations are used to create 3D visualizations.
Keywords
aerospace simulation; attitude control; control system synthesis; feedback; motion control; space vehicles; 3D visualization; computer simulation; control system design; feedback law; rotational motion control; spacecraft formation simulation; translational motion control; Aerodynamics; Computational modeling; Computer simulation; Control system synthesis; Data visualization; Earth; Feedback; Motion control; Quaternions; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics, 2008. IECON 2008. 34th Annual Conference of IEEE
Conference_Location
Orlando, FL
ISSN
1553-572X
Print_ISBN
978-1-4244-1767-4
Electronic_ISBN
1553-572X
Type
conf
DOI
10.1109/IECON.2008.4757939
Filename
4757939
Link To Document