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A new tension control law for deployment of tethered satellites

โœ Scribed by S. Pradeep

Book ID
108393734
Publisher
Elsevier Science
Year
1997
Tongue
English
Weight
372 KB
Volume
24
Category
Article
ISSN
0093-6413

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The dynamics of a tethered satellite system (TSS) during deployment and retrieval in orbit are considered. The system consists of a space station and a second body (a sub-satellite) connected to it by a tether. The station and sub-satellite are assumed to be point masses whose mass centre describes