FIELD: instrument making.
SUBSTANCE: invention relates to payload for differential correction satellite. For this purpose, load comprises inlet channel (201, 202, 503) for receiving navigation signals transmitted at least by one ground navigation station (NLES) in first frequency range, and multiple output channels (206, 207, 208, 216, 217, 218), each of which is intended for transmission of navigation signals in frequency range different from said first range and from other ranges translation, characterised by that it additionally contains navigation processor (501).
EFFECT: technical result is providing of useful or semitransparent payload for satellite, which enables to perform task of transparent relay of satellite navigation messages and differential correction messages and simultaneously introduced some specific types of processing at the level of satellite, allowing to increase safety, ensure continuity of service integrity control, as well as efficiency of radio communication.
20 cl, 7 dwg
Authors
Dates
2016-08-27—Published
2012-07-20—Filed