Experimental verification of possibility of spacecraft initial orbit determination using radial velocity measured by one measuring point

1Sheptun, AD, 2Ivanov, OM, 2Mashtak, IV
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
2Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2001, 7 ;(Supplement1):092-097
https://doi.org/10.15407/knit2001.01s.092
Publication Language: Russian
Abstract: 
The main fundamentals of methodology to determine of spacecraft (SO initial orbit using radial velocity measured by a ground-based measuring point are given. The concrete data of this methodology experimental verification are presented here. These data were obtained at full-scale test using Sich-1 SC navigation measurements. It is made an analysis of obtained results.