首页 | 本学科首页   官方微博 | 高级检索  
     检索      

用于飞控系统分析的辅助根轨迹法
引用本文:李朝晖.用于飞控系统分析的辅助根轨迹法[J].飞行力学,1999,17(1):59-64.
作者姓名:李朝晖
作者单位:中国飞行试验研究院,西安,710089
摘    要:借助于微型计算机及C语言开发环境下的丰富作图功能和快速运算能力,通过引入计算机根轨迹方法之一的分支跟踪法,从飞控系统的开环极点出发,通过矢量搜索,逐步求取根轨迹分支上满足辐角条件的点。由于其搜索过程的收敛和唯一性,因而其计算速度远高于网格搜索等方法。

关 键 词:计算机辅助根轨迹法  分支跟踪法  飞控系统
修稿时间:1998年6月16日

The Method of Computer-Aided Root-Locus for Analysis of Flight Control System
Li,Zhaohui.The Method of Computer-Aided Root-Locus for Analysis of Flight Control System[J].Flight Dynamics,1999,17(1):59-64.
Authors:Li  Zhaohui
Institution:Chinese Flight Test Establishment
Abstract:With the help of microcomputer and its powerful calculation with the graphic library in C language, one of the computer aided root locus methods, approach to branch tracking, is introduced into determining by vector locating step by step root points consistent with the spoke argument condition based upon pole points for flight control system. With the convergence and uniqueness on the vector locating, so its processing is much faster than the net method or other's; also only with the pole points for an open system, so not concerning about how branching for root loci of the system. The approach to branch tracking is especially favorable to those systems with pure time delay since there is no any difference substantially when it is applied to and processes the systems with or no pure time delay.Also in this paper several examples for flight control system are given so as to show and identify its effectiveness and accuracy.
Keywords:Computer  aided root  locus method    Approach to branch tracking Flight control system
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号