DAMPING SYNTHESIS AND DAMPED DESIGN FOR FLEXIBLE SPACECRAFT STRUCTURES

被引：1

|

作者：

SONI, ML

KLUESENER, MF

DRAKE, ML

机构：

来源：

COMPUTERS & STRUCTURES | 1985年 / 20卷 / 1-3期

关键词：

D O I：

10.1016/0045-7949(85)90104-X

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

引用

收藏

页码：563 / 574

页数：12

相关论文

共 50 条

[1] QFT design for spacecraft with uncertain flexible structures
Chen, Wen-Hua
WCICA 2006: SIXTH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION, VOLS 1-12, CONFERENCE PROCEEDINGS, 2006, : 8191 - 8195
[2] Parametric synthesis of the design of a flexible and deformable spacecraft
Litvinov, ND
JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2000, 39 (01) : 139 - 147
[3] INTEGRATED CONTROLS - STRUCTURES DESIGN METHODOLOGY FOR FLEXIBLE SPACECRAFT
MAGHAMI, PG
JOSHI, SM
PRICE, DB
JOURNAL OF SPACECRAFT AND ROCKETS, 1995, 32 (05) : 839 - 844
[4] REAL TRANSFORMATION FOR MODAL ANALYSIS OF FLEXIBLE DAMPED SPACECRAFT
HABLANI, H
SHRIVASTAVA, S
ACTA ASTRONAUTICA, 1979, 6 (5-6) : 615 - 630
[5] On the design of flexible spacecraft
Litvinov, ND
JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2001, 40 (02) : 314 - 339
[6] Active damping control of flexible appendages for spacecraft
Zhang, Yizhe
Guan, Xin
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 75 : 237 - 244
[7] Modal damping optimization for general damped structures
Wei, Yong
Chen, Guo-Ping
Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2006, 19 (04): : 433 - 437
[8] STABILIZATION OF WEAKLY DAMPED FLEXIBLE STRUCTURES
BERRAHMOUNE, L
RAIRO-AUTOMATIQUE-PRODUCTIQUE INFORMATIQUE INDUSTRIELLE-AUTOMATIC CONTROL PRODUCTION SYSTEMS, 1990, 24 (04): : 301 - 321
[9] STABILITY OF LARGE FLEXIBLE DAMPED SPACECRAFT MODELED AS ELASTIC CONTINUA
MAHARANA, PK
SHRIVASTAVA, SK
ACTA ASTRONAUTICA, 1984, 11 (02) : 103 - 109
[10] Aerodynamic damping for flexible structures
Kaiser, K
WIND ENERGY CONVERSION 1997, 1997, : 97 - 100

← 1 2 3 4 5 →