Model Reference Variable Structure Autopilot Design for Homing Missile

摘要

To design the control system for some homing missile so that the autopilot can trans- fer guidance command correctly and be robust to disturbances, such as the measurement noises and parameter variation caused by areodynamic floating. The model reference adaptive control was combined with the variable structure control to design a model reference variable structure (MRVS) control system whose control structure is simple and can be realized easily. The simu- lation results indicate that MRVS can complete the task of transferring guidance command and suppress the distrubances effectively.