RESPONSE OF LARGE SPACE STRUCTURES WITH STIFFNESS CONTROL.

Jay Chung Chen*

*Corresponding author for this work

Research output: Chapter in Book/Conference Proceeding/ReportConference Paper published in a bookpeer-review

Abstract

For large space structures, such as the 100-meter-diameter wrap-rib deployable antenna and spinning solar sail, whose out-of-plane stiffness is derived from in-plane tension, the out-of-plane motion can be actively controlled by time-varying in-plane tension. An elastic string is used to demonstrate the proposed approach, which results in a nonlinear ordinary differential equation. An approximation method is outlined from which the magnitude of time-varying tension can be determined based on the efficiency factor, the time factor or the optimal factor.

Original languageEnglish
Title of host publicationAdvances in the Astronautical Sciences
EditorsG.T. Tseng, Peter M. Bainum, David A. Levinson
Publisherr American Astronautical Soc by Univelt Inc
Pages417-431
Number of pages15
EditionPt 1
ISBN (Print)0877031908
Publication statusPublished - 1984
Externally publishedYes

Publication series

NameAdvances in the Astronautical Sciences
NumberPt 1
Volume54
ISSN (Print)0065-3438

Fingerprint

Dive into the research topics of 'RESPONSE OF LARGE SPACE STRUCTURES WITH STIFFNESS CONTROL.'. Together they form a unique fingerprint.

Cite this