摘要
对非线性控制的逆系统方法原理进行了介绍,将该方法应用于空空导弹制导设计中,设计了导弹质心运动动力学系统的控制器,该控制器通过对弹道坐标系下导弹的纵向过载和法向过载实施控制,可使导弹在控制系统中的速度、偏航角和俯仰角输出信息渐近跟踪制导指令,以实现空空导弹对攻击目标的跟踪。
The inverse system method of nonlinear control is introduced, and its theory is applied to the guidance design of airtoair missiles. A controller used in a missile dynamics system of the centroid motion is designed. The output informations of control system, including velocity, yaw angle and pitching angle, can keep the track of the guidance command. The progressive tracking control is realized by controlling the longitudinal and normal gload of the missile.
出处
《飞行力学》
CSCD
2003年第3期45-47,70,共4页
Flight Dynamics
基金
航空科学基金资助项目(97D53037)
