THE HIGH-APOGEE ARTIFICIAL SPACECRAFT ASTROPHOTOMETRICAL AND ASTROMETRICAL OBSERVATIONS IN THE SAYAN MOUNTAINS OBSERVATORY OF ISTP SB RAS AND THEIR APPLICATIONS TO CHECKING THE SPACECRAFT STATE OF OPERATIONV.Goryashin1, Yu.Karavaev1, M.Mishina1, M.Eselevich1, T.Tsukker1, V.Tergoev1,O.Yurysheva1, P.Papushev1, R. Kopyatkevich2, G.Mishin2, P.Shaburov2, N. Sakva2 1 Institute of Solar-Terrestrial Physics (ISTP), Sibirian branch of Russian Academy of Sciene, Irkutsk, p.b. 4026, Russia 664033
2 Central Research Institute of Machine Building, (THNIIMASH), Korolev, Moscaw region, Pionerskaya 4,Russia
In this report we will present and discuss the methods, facility and results astrophotometrical
and astrometrical observations of a high-apogees artificial spacecrafts at Sayan mounting
observatory (operated by the ISTP SB RAS). The observations started from the second half of
the 20-th century and have been continued up to the present time. The observations facility
used in the of the high-apogees artificial satellites observations are three automated telescope
with diameters 0.5, 0.6 and 1.7 meters and equipment for astrometrical and astrophotometrical
measurements in visual and infrared bands. As far as an astrometrical measurements,
measurements of position of the satellite concerning to stars in a field of view we shall discuss
sufficiency of the achieved accuracy of measurements for definition of the current orbits and
its evolution under action of various factors of the space environments and spacecrafts
design.
The astrophotometrical data are light curves of a spacecrafts recorded by a broad band
astrophotometers with high temporal resolution. Description and systematization of
observational data has been made. The interpretation of the obtained light curves must be
performed using a mathematical modeling of surface geometry and optical parameters of the
satellites. The analysis of results of the dynamic phenomena during rotation uncontrolled
geostationary satellites are considered. The opportunity of research of the spacecrafts
technical condition and its launching facility is considered. Physical mechanisms of changes
orbital and proper rotation motion parameters are discussed.
Размещен 29 ноября 2006.
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