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.
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