摘要
本文分别用状态变量及传递函数优化法定量确定了飞机性能指标和控制规律,并用仿真研究下机载数字机实现其规律的实时问题。
A method for computing the control law and the performance index of the flight control system using the optimization techniques of the state variable and transfer function has been discussed in this paper, and the control law has been verified by real-time simulation on the computer. The results showed quite good.
出处
《五邑大学学报（社会科学版）》
1987年第1期27-36,共10页
Journal of Wuyi University(Social Sciences Edition)
