Behaviour of spacecrafts group injecting by one laungh vehicle

Heading: 
Spacecraft Dynamics and Control
1Paltsev, NG
1Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2001, 7 ;(Supplement1):097-100
https://doi.org/10.15407/knit2001.01s.097
Publication Language: Russian
Abstract: 
A behaviour of compact group of passive spacecrafts (SO injecting by one launch vehicle under the influence of terrestrial gravity forces is considered. It is shown that the stability of SC depends on the type of separation system, the method and the direction of SC separation. This one so depends on orientation accuracy of SC last stage, which determined initial SC group configuration.
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References: 
1. Sochilina A. S. On identification of geosynchronous satellite in accordance with their initial circular orbits. Nabljud. iskusstv. nebes. tel, No. 85, 104—110 (1990) [in Russian].