A Spin Missile Autopilot Designed Using Dynamic Inversion

Dynamic model of a spin missile was established in pseudo body coordinates.A three axes autopilot based on dynamic inversion control with output redefine was developed for it.The design method for parameters was also in- volved.Numerical simulations showed that this autopilot is of good performance and robustness.This autopilot is sim- ple structured and its parameters are easy to be determined.