It is an innovative try to control hypersonic bank-to-turn missiles using the deflectable nose and flaps. The high-er control efficiency, faster response, better stability and compactness of the nose control are shown by comparing the de-flectable nose control with the normal tail fin control. A mathematical model of the missile, which is time-varying, non-linear and strong coupling, is establihsed by multi-body dynamics to be used for designing the controller. A robust con-troller of deflectable nose control is designed by variable structure control theory, selecting sliding mode surfaces with tracking error and its integral function, and considering parameter disturbance of the model. The simulation results show the controller can response quickly and track precisely. The deflectable nose control is proper for the bank-to-turn missile.