摘要：The problem of satellite formation tracking control is studied by using the tool, the satellite tool kit （STK ） *** fight against gravitational perturbation rejection, a sliding mode controller for each satellite is proposed to accomplish the orbit trace and is then verified by the *** the purpose of accomplishing the formation tracking mission with bidirectional communication in STK,a time-share orderly calling plug-in is designed by C ＋＋,which gives solutions to the problems of the monopolization of computing resource and no return of the satellite identifier in the calculation center. The effectiveness of the decoupling approach is tested and verified by the *** simulation results obtained by the STK are more meaningful than those obtained by Matlab.