摘要
研究了对接包线内伸缩套管的建模和控制问题。建立了大气扰动中的伸缩套管模型,采用H∞方法设计了伸缩套管的控制律,并进行了仿真。仿真结果表明,在该控制律作用下,伸缩套管系统具有良好的跟踪能力,抗干扰性能提升了1个数量级。
The problems of modeling and control of the flying boom in its connection envelope are studied in this paper. The model of the boom in atmospherics is constructed, and then its control law is designed with the H∞ method. Furthermore, the simulations of the pitch angle and roll angle of the boom are made, and the results show that the boom system under the control law has a perfect performance of command - tracking and the capability of jamming resistance is upgraded about 10 times.
出处
《飞行力学》
CSCD
北大核心
2008年第4期14-18,共5页
Flight Dynamics
