电光与控制, 2011, 18 (6): 62, 网络出版: 2011-06-24
超音速巡航导弹飞行高度的串级控制与仿真
Simulation and Cascade Control of Supersonic Cruise Missile Flight Altitude
摘要
建立了超音速巡航导弹飞行高度的串级控制系统模型;利用最优参数整定法设计了副回路反馈补偿PD调节器;运用Matlab/Sisotool设计了主回路控制器。仿真结果表明,串级控制能较大程度地提高超音速巡航导弹飞行高度的控制性能。
Abstract
The cascade control system model of supersonic cruise missile was established at first.Then,a vice loop feedback compensation PD adjuster was designed by using optimal parameter setting method and a main loop controller was designed by use of Matlab/Sisotool.The results of simulation showed that the cascade control can greatly improve the control performance of supersonic cruise missile flight altitude.
江秀强. 超音速巡航导弹飞行高度的串级控制与仿真[J]. 电光与控制, 2011, 18(6): 62. JIANG Xiuqiang. Simulation and Cascade Control of Supersonic Cruise Missile Flight Altitude[J]. Electronics Optics & Control, 2011, 18(6): 62.