Aircraft three-axis attitude control system and method based on active flow control

The invention discloses an aircraft three-axis attitude control system and method based on active flow control. A flying wing layout aircraft is used as an application carrier, and various active flowcontrols such as jet thrust vector, circulation control and reverse blowing are cooperatively used, so that three-axis attitude control of the aircraft in pitching, rolling and yawing directions is realized, and the maximum control moment which can be generated by a traditional control surface is reached or even exceeded. The system has the advantages that the structural arrangement is simple, adverse effects of engine shutdown and the like on active flow control are avoided, and the reliability of the system is improved. The response speed of the active flow control is higher than that of control surface control, and the maneuvering characteristics of the aircraft can be effectively improved. 本发明公开了一种基于主动流动控制的飞行器三轴姿态控制系统及方法，以飞翼布局飞行器为应用载体，协同使用射流推力矢量、环量控制和反向吹气多种主动流动控制，实现了飞行器俯仰、滚转、偏航方向上的三轴姿态控制，并且达到甚至超过了传统舵面所能产生的最大控