Title
Deployment of Long-measured Flexible Structure in Orbit
Authors
Year of publication
2014
Published in
Article type
scientific article
Publication language
english
Keywords
EN
- spacecraft
- pantograph structure
- deployment
Abstract
EN Dynamics of the spacecraft with giro-gravitational system of stabilisation, in which the pantograph design deployed in an orbit and containing on the end the concentrated mass is used as the gravitational stabilizer and the carrier of solar batteries, is investigated. The analysis of the obtained information is carried out and graphs that illustrate behaviour of characteristic variables are discussed.
Pages (from - to)
335 - 342
License type
CC BY (attribution alone)
Full text of article
Access level to full text
public
Ministry points / journal
5
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