摘要
本文给出的非线性控制系统实的第二标准型绝对稳定的显式准则,包含并改进了文[1]所得到的判别准则.将本文准则应用于著名的飞机纵向运动方程,所得结果包含并改进了文[1,2,3,4]中所得到的相应结论.
In this paper, some explicit criterions of absolute stability for the trivial solution of the real second canonical form of non-liaear control system are given, which include and improve the criterions in paper[l]. By applying these criterions to the well-known equation of the longitudinal motion of aircraft, some results are obtained, which include and improve the corresponding results in papers [1,2,3,4].
出处
《应用数学和力学》
CSCD
北大核心
1993年第5期445-454,共10页
Applied Mathematics and Mechanics
关键词
非线性
控制系统
绝对稳定性
autonomous system, non-linear control system, equation of motion, positive definite function, absolute stability