SPACECRAFT STRUCTURAL MODEL IMPROVEMENT BY MODAL TEST-RESULTS

被引：4
作者：
CHEN, JC
PERETTI, LF
GARBA, JA
机构：
[1] JPL, Pasadena, CA, USA, JPL, Pasadena, CA, USA
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 1987年 / 24卷 / 01期
关键词：
This research was carried out by the Jet Propulsion Laboratory; California Institute of Technology; under Con- tract NAS7-918. This task was sponsored by Samuel L. Ven-neri; NASA Office of Aeronautics and Space Technology;
D O I：
10.2514/3.25878
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
16
引用
收藏
页码：90 / 94
页数：5
相关论文
共 16 条
[1]   OPTIMIZATION PROCEDURE TO CORRECT STIFFNESS AND FLEXIBILITY MATRICES USING VIBRATION TESTS [J].
BARUCH, M .
AIAA JOURNAL, 1978, 16 (11) :1208-1210
[2]   THEORY OF INCOMPLETE MODELS OF DYNAMIC STRUCTURES [J].
BERMAN, A ;
FLANNELLY, WG .
AIAA JOURNAL, 1971, 9 (08) :1481-+
[3]  
BERMAN A, 1982, AIAA820743 PAP
[4]   ANALYTICAL MODEL IMPROVEMENT USING MODAL TEST-RESULTS [J].
CHEN, JC ;
GARBA, JA .
AIAA JOURNAL, 1980, 18 (06) :684-690
[5]  
CHEN JC, 1984, AIAA841051 PAP
[6]  
CHEN JC, 1983, AIAA830812 PAP
[7]  
CHEN JC, 1984, 2ND P INT MOD AN C S, P796
[8]  
CHEN JC, 1984, AIAA841069 PAP
[9]   STATISTICAL IDENTIFICATION OF STRUCTURES [J].
COLLINS, JD ;
HART, GC ;
HASSELMAN, TK ;
KENNEDY, B .
AIAA JOURNAL, 1974, 12 (02) :185-190
[10]  
DOBBS MW, 1981, SAE811050 PAP
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