摘要
本文给出非线性控制系统实用的策二标准型平凡解绝对稳定的显武准则,包含并改进了廖晓昕(1982)所得到的充分性准则。将所得结果应用于著名的飞机纵向运动方程,所得结果包含并改进了廖晓昕、王慕秋、Michel A N所得到的相应结论。
In this paper, Some practical criterions of absolute stability for the trivial solution of the second canonical form of non-linear consrol system are given, which include and improve the criterions given by Liao Xiao-xin (1982). By applying these critirions to the well known equation of the longitudinal motion of aircraft, some results are obtained, which include and improve the corresponding results given by Liao Xiao-xin, Wang Mu-qiou and Michel, A. N..
出处
《山东矿业学院学报》
CAS
1990年第3期306-313,共8页
Journal of Shandong University of Science and Technology(Natural Science)
关键词
飞机
控制系统
运动方程
稳定性
autonomous system
non-linear control systems
aerodynamics
aeroplanes
equation of motion
positive definite function
