摘要
本文在文献［１］、［４］的基础之上针对线性系统提出了一种切换超平面的鲁棒设计法。该方法考虑了系统参数的变化，具有强的鲁棒性。设计实例给出了将该方法用于某型海防导弹高度控制回路的仿真结果，其结果是相当令人满意的。
On the basis of the reference 1 and 4 and in connection with a linear sysytem, a robust design method for the switching hyperplane is proposed. The design has more strong robustness due to considering the variance of the system parameters. An altitude control loop of a certain marine-defence missile is regarded as a design example, whose simulation results shows the design to be very satisfide.
出处
《航天控制》
CSCD
北大核心
1994年第2期1-10,共10页
Aerospace Control
