Sliding mode control of concomitant satellites´ formation tracking via STK

Author

Chen Yangyang ; Zhang Guoxi ; Feng Yuan ; Wei Ping

Author_Institution

Sch. of Autom., Southeast Univ., Nanjing, China

fYear

2014

fDate

28-30 July 2014

Firstpage

344

Lastpage

348

Abstract

This paper considers the formation tracking control problem of concomitant satellites by using STK (Satellite Tool Kit). A new sliding mode control protocol which is suitable to fight against the gravitational perturbation is proposed to achieve the robust tracking around the given orbit. Information flows are able to be translated in STK simulations by using the time-share scheme. The effective of the decoupling approach is tested and verified by STK, which is more meaningful than the results obtained by MATLAB.

Keywords

artificial satellites; mathematics computing; perturbation techniques; robust control; variable structure systems; MATLAB; STK simulations; concomitant satellite formation tracking control problem; decoupling approach; gravitational perturbation; information flows; robust tracking; satellite tool kit; sliding mode control protocol; time-share scheme; Computational modeling; Educational institutions; Mathematical model; Orbits; Satellites; Sliding mode control; Tracking; Concomitant Satellites; Decoupling Approach; Formation Tracking; Satellite Tool Kit; Sliding Mode Control;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2014 33rd Chinese

Conference_Location

Nanjing

Type

conf

DOI

10.1109/ChiCC.2014.6896646

Filename

6896646