导弹制导控制一体化技术是将制导系统和控制系统综合进行设计,可以充分发挥导弹的整体性能,提高命中精度。为了加强毁伤效果,考虑落角约束是一体化设计中的热点研究问题。针对倾斜转弯导弹,首先,建立了导弹运动模型和弹目相对运动模型,这是一体化研究的基础；随后,对现有研究方法进行分类和归纳；最后,梳理了目前制导控制一体化研究存在的问题以及发展趋势。

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.