In the presented work the questions of application of satellite navigationals are considered with their differential additions for the high-fidelity navigation of objects of space-based having an elliptic type of orbit. It is rotined that application of traditional differential methods to this category of users does not result in the increase of authenticity of the got navigation decisions. A method over of estimation of the height distributing of electronic concentration of ionosphere is brought, which allows to get distributing of electronic concentration not only on co-planar co-ordinates but also on a height, his experimental approbation is carried out.
satellite radio engineering navigation system, differential method, ionosphere error, elliptic orbit
"Prymenenye metoda formyrovanyia dyfferentsyalnыkh popravok dlia apparaturы sputnykovoi navyhatsyy kosmycheskykh apparatov vydovoho nabliudenyia" ,
Scientific Works of Kharkiv National Air Force University,