The integrated missile guidance and control technology is to design the guidance system and the control system of the missile comprehensively, which can fully exploit the overall performance of the missile and improve the hit accuracy.Taking the terminal angle constraint into consideration is a hot spot of research in the integrated design in order to enhance the damage effect.For bank to turn missile, the missile motion model and the missile-to-target relative motion model are established at first, which is the basis of the integrated research;the existing research methods are classified and summarized subsequently;and the problems and development trends of the current integrated guidance and control research are sorted out in the end.