Preliminary specification of spacecraft orbital elements by moment of separation based on one measurement session

Heading: 
Spacecraft Dynamics and Control
1Koshevoi, OV
1Spacecraft Flight Control Center Evpatoria, Ukraine
Kosm. nauka tehnol. 2001, 7 ;(Supplement1):072-073
https://doi.org/10.15407/knit2001.01s.072
Publication Language: Russian
Abstract: 
Problems of the ballistic-navigational support of spacecraft operating in the primary flight stage within the one-point technology are considered. The method of approximate estimation of the motion parameters based on one measurement session is proposed.
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References: 
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