<link rel="stylesheet" href="styles.cf390c6bfbe7555f.css">

校內出版品;;Campus Publications

Permanent URI for this communityhdl:11536/12

除個人與團體研究發表外，校內單位同時出版了不少學術專業出版物，諸如交通大學出版社與科技法學評論等項。;;Collections from Pulishers in NCTU with Professional Research Publications like NCTU Press, etc.

Browse

Filters

1966 - 19696

Settings

🏛️國立陽明交通大學機構典藏

Author: search.filters.author.韓光渭End date: 1969

Search Results

Now showing 1 - 6 of 6
  • Thumbnail Image
    Item type:Item,
    Analysis of Linear Control Systems with Transpsort Lage
    (交大學刊編輯委員會, 1969-04)
    陳永國
    ;
    韓光渭
    ;
    Y.K.Chen
    ;
    K.W.Han
    A control system, contacting a transport lag is usually difficult for analysis, due to the existence of a transcedental function in the system characteristic equation. Yaohan Chu had presented a phase- angle- loci method, but it becomes increasingly difficult for higher order systems.(1)Eisenberg had given a fairly nice method, but it has been applied only to systems containing one transport lag.(2) In this paper , the root locos method is applied to the analysis of linear control systems with transport lags. The basic approach is to use the special property of zero-order holding circuit to represent a linear control system with transport lag by an equivalent sampled-data control system, then the system stability is analyzed in Z-domain using root-locus method.
  • Thumbnail Image
    Item type:Item,
    Stability Analysis of Nonlinear Reactor Control Systems
    (交大學刊編輯委員會, 1968-10)
    韓光渭
    ;
    陳英亮
    ;
    K.W.Han
    ;
    Y.L.Chen
    A method for testing control system stability is presented, which is useful ror finding the limit cycles of high order systems with multiple nonlinearities. The presented method is applied to the analysis of the control system of a material testing reactor, and a comparison with the method in a current literature is given.
  • Thumbnail Image
    Item type:Item,
    Analysis and Design of Control Systems for Aircraft and Missiles
    (交大學刊編輯委員會, 1966-04)
    韓光渭
    ;
    K. W. Han
    In this paper, control systems for aircraft and missiles are analyzed and designed using a "stability curve" method which is particularily suitable for testing stability and adjusting parameters for complex control systems. Design procedures are given along with examples.
  • Thumbnail Image
    Item type:Item,
    Stability Analysis of High Order Systems With Multiple Nonlinearities
    (交大學刊編輯委員會, 1967-04)
    韓光渭
    ;
    K.W.Han
    A method of testing stability in high order systems with multiple nonlinearities is presented. The presented method can be used to find the limit cycles and the relative stability characteristics of a system. A control system for satellite attitude stabilization is considered, and a system with three nonlinearities is analyzed.
  • Thumbnail Image
    Item type:Item,
    Analysis of Nonlinear Sampled-Data System Using Z-Transform Method
    (交大學刊編輯委員會, 1966-10)
    陳英亮
    ;
    韓光渭
    ;
    Y.L.Chen
    ;
    K.W.Han
    A method of testing stability of sampled-data systems with a relay-type nonlinearity is presented. In the z-domain, a linear sampled-data system which is equivalent to a nonlinear system under steady state condition can be found, and the existence as well as the stability characteristics of the limit cycle can be defined.
  • Thumbnail Image
    Item type:Item,
    Analysis of Sampled-Data Systems in the W-plane
    (交大學刊編輯委員會, 1966-10)
    韓光渭
    ;
    孫志凱
    ;
    K.W.Han
    ;
    C.K.Sun
    A computer program for doing bilinear transformation is presented, and the relations between z-plane and w-plane are investigated. Various methods for analyzing sampled-data control systems in the w-plane are considered.