摘要
将非线性无源方法用于导弹纵向机动飞行控制,并通过变结构控制器补偿系统的不确定性,这样设计的控制器能保证系统的鲁棒稳定性。将此方法用于导弹地形跟踪控制,仿真结果表明:此方法在导弹纵向机动飞行中控制效果较好。
In this paper, the passivity-based control method is applied to the missile longitudinal maneuvering flight control and the compensatory controller is designed using the variable structure control techniques which deal with uncertainties of a system. The method ensures robust stability of the control system.The control laws are used in terrain following. The simulation results show that the control laws have better for missiles during longitudinal maneuvering flight conditions.
出处
《飞行力学》
CSCD
2004年第1期56-59,共4页
Flight Dynamics
