摘要:AbstractThis paper deals with the autopilot design for a 155-mm dual-spin projectile equipped with a course correction fuze (CCF). This class of projectiles is subject to high nonlinearities and to strongly coupled dynamics between its pitch and yaw channels. To overcome these difficulties a Nonlinear Dynamic Inversion (NDI) based autopilot is proposed. This autopilot possesses a cascade structure where an inner loop linearises the nonlinear system dynamics and an outer loop enables to impose the desired system closed-loop dynamics. The configuration of a dual-spin projectile requires the development of two separate control loops, one for the roll channel and another for the pitch/yaw channels. The pitch/yaw controller is developed under a Time Scale Separation (TSS) scheme. This not only helps to accelerate the design of the control laws but also to achieve a satisfactory level of robustness. The autopilots are also validated with a nonlinear 7-DOF simulation.