Design and Simulation of the Rolling Loop for a Gliding Missile with High Aspect Ratio Wings

The rolling loop of a certain gliding missile with high aspect ratio wings (HARW) was designed through the introduction of the lateral overload feedback on the basis of the traditional Skid-to-Turn (STT) control mode, the equation of the centripetal force in our system was constructed, and the six degree-of-freedom (six-DOF) nonlinear mathematical simulation and semi-physical simulation were performed. The track of the rolling angle to the lateral overload was realized, the sideslip angle during turning process was decreased, and the ability resistant to rolling disturbance of HARW missile was enhanced.