Title :
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
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;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896646
