Article 15112

Title of the article

DETERMINING HIGH-SPEED PARAMETERS OF SPACE VEHICLES BY NON-ABATEMENT MEASUREMENTS IN THE INFORMATION BROADCASTING SYSTEM  

Authors

Chaplinsky Vladimir Stepanovich, Doctor of engineering sciences, professor, Senior staff scientist, Research Institute of Space Systems named after A. A. Maksimov – branch of “State Space Research and Production Center named after M. V. Khrunichev” (Yubileyny, Moscow region), chvs2006@mаil.ru
Shastitko Vasily Alexandrovich, Postgraduate student, Research Institute of Space Systems named after
A. A. Maksimov – branch of “State Space Research and Production Center named after M. V. Khrunichev”
(Yubileyny, Moscow region), niiks@khrunichev.com
Afanasyev Dmitry Yuryevich, Postgraduate student, Research Institute of Space Systems named after A.A.Maksimov – branch of “State Space Research and Production Center named after M.V. Khrunichev”
(Yubileyny, Moscow region), niiks@khrunichev.com
Tyurin Mikhail Vladimirovich, Chief line designer, Research Institute of Physical Measurements (Penza), info@niifi.ru

Index UDK

621.396

Abstract

The article substantiates the structure of high-speed navigating parametres of space vehicles - subscribers of space system of information relay, which can be defined by non-inquiry measurements of a bearing frequency of accepted radio signals.

Key words

space system of relay, satellite-retransmitter, spacecraft, radio line, radial pseudo-speed.

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Дата создания: 26.08.2014 08:52
Дата обновления: 26.08.2014 15:15