Article 13213

Title of the article

                                   SECURING GLOBAL AND OPERATIVE CONTROL AND DIRECTION                                         OF UPPER-STAGE ROCKETS OF A SPACE CRAFT 

Authors

Konovalov Vladislav Petrovich, Candidate of engineering sciences, principal researcher worker, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev (Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com
Makatrov Aleksandr Sergeevich, Candidate of engineering sciences, senior researcher worker, deputy director, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev (Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com
Bogdanov Sergey Anatol'evich, Engineer, head of the complex, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev
(Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com
Gerastovskiy Vyacheslav Fedorovich, Engineer, deputy head of the complex, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev (Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com
Kutsevalov Aleksandr Timofeevich, Candidate of engineering sciences, senior researcher worker, head of department, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev (Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com
Chaplinskiy Vladimir Stepanovich, Doсtor of engineering sciences, professor, principal scientific worker, Spaсe Systems Research Institute named after A. A. Maksimov – branch of the State Research and Production Space Center named after M. V. Khrunichev (Moscow, 18 Novozavodskaya str.), niiks@khrunichev.com 

Index UDK

629.786.2.05 (075.8) 

Abstract

Control over the execution of a program of spacecraft orbital injection and estimation of upper-stage rocket on-board systems functioning is carried out on the basis of telemetric and trajectory data, received and processed by means of a ground inspection center, located on the territory of a country. At that the most crucial sectors of upper-stage rocket cruise engines’ ignition take place beyond the radiovisibility of the ground center. The authors consider the problems of increasing the operative and global rate of telemetric and trajectory control of upper-stage rockets of space crafts via application of space-based relay and navigation systems, as well as the opportunities of using ground inspection centers not only for flight control, but also for directing the perspective upper-stage rockets. A multifunctional space-based relay system, which is being developed in Russia on the basis of the new generation of relay satellites “Luch-5” and “Luch-4”, will enable the continuous control over the flight of upper-stage rockets after separation from a carrier rocket on the support orbit during their transfer to the intermediate and transfer orbits at the altitude up to 2000 km, and in the higher sectors of zones of directional patterns of restranslating satellites’ antennas. The orbits of space craft injection to higher orbits are located in the zone of dicrete radio-navigation field of the space navigation systems. To determine the parameters of such orbits there is a technology combining determination of movement parameters by observations in the continuous navigation field with subsequent adjustment thereof according to the measurements in the discrete radio-navigation field. Joint application of external trajectory data, received by the equipment of space navigation
system user, and inertial navigation system data increases authenticity of equipment of a space navigation system user and inertial system precision. After the execution of upper-stage rocket control relay modes the ground inspection center may be reorganized into a ground inspection and control center, elaborating and transferring commands to the upper-stage rockets, counteracting denials and deviations from a flight program. 

Key words

control, space rocket, carrier rocket, upper stage rocket, telemetric data, trajectory data, multi-purpose data relay system, space navigation systems, user navigation equipment, relay satellite. 

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References

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Дата создания: 28.08.2014 10:35
Дата обновления: 28.08.2014 11:43