The main motivity analysis of deployment process of Astromesh

被引：0

作者：

Chen, Guohui ^{[1
]}

Xiao, Yong ^{[1
]}

Lei, Yanni ^{[1
]}

机构：

[1] China Acad Space Technol Xian, Xian 710100, Peoples R China

来源：

FRONTIERS OF GREEN BUILDING, MATERIALS AND CIVIL ENGINEERING, PTS 1-8 | 2011年 / 71-78卷

关键词：

Astromesh; deployment; coordinate; torque motor; synchronous drive mechanism hinge;

D O I：

10.4028/www.scientific.net/AMM.71-78.1554

中图分类号：

TU [建筑科学];

学科分类号：

0813 ;

摘要：

The deployment process of Astromesh is analyzed and the basic unit is defines, based on which overall coordinate system of Astromesh and the units local coordinate system are established. The role of synchronous drive mechanism hinges and motor are analyzed in the unit local coordinate system, and whose action principle is stated in the form of parameter.

引用

页码：1554 / 1559

页数：6

共 4 条

[1]

HE XS, 2005, THEORETICAL MECH

[2] In-orbit deployment characteristics of large deployable antenna reflector onboard Engineering Test Satellite VIII [J].

Meguro, Akira ;

Shintate, Kyoji ;

Usui, Motofumi ;

Tsujihata, Akio .

ACTA ASTRONAUTICA, 2009, 65 (9-10) :1306-1316

[3]

Thomson M. W., 1999, IEEE Antennas and Propagation Society International Symposium. 1999 Digest. Held in conjunction with: USNC/URSI National Radio Science Meeting (Cat. No.99CH37010), P1516, DOI 10.1109/APS.1999.838231

[4]

Thomson Mark W., 20 AIAA INT COMM SAT

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