A Full-trajectory Design Method for a Waverider Hypersonic Vehicle with Boost-glide-attack Process

A guidance controller is designed for the boost-glide waverider hypersonic vehicle, which can meet the requirements of the whole flight. The task of reaching the desired altitude and velocity at the end of the boost phase will be achieved through the controller. So that the vehicle can perform long distance maneuvers in the condition of quasi-balanced glide, and finally dive to hit the target. The performance of the controller is verified by simulation. The guidance controller can make the hypersonic vehicle to complete the flight task and meet the control requirements of hypersonic vehicle maneuver.