Vibroimpact Dynamics of a Tethered Satellite System
Joint Authors
Source
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-11-21
Country of Publication
Egypt
No. of Pages
12
Main Subjects
Abstract EN
This paper presents the vibroimpact dynamics of an in-plane tethered subsatellite caused by sudden braking during deployment or retrieval.
The full dynamics of the subsatellite are composed of its free-flight and the instantaneous impacts.
At the moment of impact, the reflective angle of the subsatellite is envisioned to be equal to its incident angle such that the impact law is obtained.
Then, the stability of the periodic vibroimpacts is analyzed using the composite Poincaré map.
Further, the vibroimpact responses that do not exceed a specified region are numerically determined via the cell mapping method.
American Psychological Association (APA)
Yu, B. S.& Wen, Hao. 2017. Vibroimpact Dynamics of a Tethered Satellite System. Shock and Vibration،Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1205134
Modern Language Association (MLA)
Yu, B. S.& Wen, Hao. Vibroimpact Dynamics of a Tethered Satellite System. Shock and Vibration No. 2017 (2017), pp.1-12.
https://search.emarefa.net/detail/BIM-1205134
American Medical Association (AMA)
Yu, B. S.& Wen, Hao. Vibroimpact Dynamics of a Tethered Satellite System. Shock and Vibration. 2017. Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1205134
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1205134