Some results of studies of the behaviour of a satellite in orbit in contingency mode under the near-Earth space influence
|1Epishev, VP, 1Isak, II, 1Kudak, VI, 1Motrunich, II, 1Noibauer, IF, 2Koshkin, NI, 3Bilinsky, AI, 3Martyniuk-Lototskij, KP, 4Blagodyr, Ya.T, 5Lopachenko, VV, 5Rykhalskij, VV, 6Ryschenko, SV, 6Zhukovetskij, AV |
1Space Research Laboratory of the Uzhgorod National University, Uzhgorod, Ukraine
2Scientific-Research Institute «Astronomical Observatory» of the I.I. Mechnikov National University of Odessa, Odessa, Ukraine
3Astronomical Observatory of the Ivan Franko National University of L’viv. L’viv, Ukraine
4Astronomical Observatory of the Ivan Franko National University of L’viv, L’viv, Ukraine
5National Center of Space Facilities Control and Test of the State Space Agency of Ukraine, Yevpatoria, AR Crimea, Ukraine
6Center of Reception and Processing of Specific Information and Control Navigation Field, Dunaivtsi, Ukraine
|Kosm. nauka tehnol. 2012, 18 ;(1):60–67|
|Section: Spacecraft Dynamics and Control|
|Publication Language: Russian|
We give some results of our analysis of the behaviour of the spacecraft EgyptSat in orbit in contingency mode as compared with free rotation parameters for other satellites. We propose a conception of an emergency situation with the object. It is shown that the integration of high-precision coordinate and photometric information obtained from different points allows one rapidly and efficiently to analyze the behaviour of spacecrafts which are in orbit without radio connection.
|Keywords: emergency situation, photometry, satellites|
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