关键词: 复合控制, 控制分配, 高阶滑模, 自适应

Abstract:  A controller design for missiles with blended lateral jets and aerodynamic is presented,The mathematical model of attitude control system in the pitch plane is constructed,and the nonlinear system theory is applied to analyze the mode. A virtual controller is designed using adaptive higher order sliding mode based on simplified mode.A constrained quadratic programming formulation is constructed considering the rate and position limits of rudder and characristic of reaction jets. Using active set methods, control allocation problem is solved.Simulation results show the effectiveness of the proposed design,which can suit the blend actuator and track the command of overload.