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|
|Publication Language: Russian|
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.