Abstract
The results of reconstruction of rotational motion of the Foton M-3 satellite during its uncontrolled flight in September 2007 are presented. The reconstruction was performed by processing the data of onboard measurements of the Earth’s magnetic field obtained by the DIMAC instruments. The measurements were carried out continuously throughout the flight, but the processing technique dealt with the data portions covering time intervals of a few orbital revolutions. The data obtained on each such interval were processed jointly by the least squares method with using integration of the equations of satellite motion relative to its center of mass. When processing, the initial conditions of motion and the used mathematical model’s parameters were estimated. The results of processing 16 data sets gave us complete information about the satellite motion. This motion, which began at a low angular velocity, had gradually accelerated and in five days became close to the regular Euler precession of an axisymmetric solid body. At the end of uncontrolled flight the angular velocity of the satellite relative to its lengthwise axis was 0.5 deg/s; the angular velocity projection onto the plane perpendicular to this axis had a magnitude of about 0.18 deg/s.
Similar content being viewed by others
References
Sarychev, V.A., Belyaev, M.Yu., Kuz’min, S.P., et al., Determination of Attitude Motion of the Salyut-6 and Salyut-7 Orbital Stations in the Slow Spin-Up Mode according to Measurement Data, Kosm. Issled., 1988, vol. 26, no. 3, pp. 390–405. [Cosmic Research, p. 336].
Sarychev, V.A., Sazonov, V.V., Belyaev, M.Yu., and Efimov, N.I., Improving Accuracy of Determination of Rotary Motion of the Orbital Stations Salyut-6 and Salyut-7 Using Measurement Data, Kosm. Issled., 1991, vol. 29, no. 3, pp. 375–389. [Cosmic Research, p. 321].
GOST (State Standard) R 25645.166-2004: Upper Atmosphere of the Earth. Density Model for Ballistic Support of Satellite Flights, 2004.
Sazonov, V.V., Chebukov, S.Yu., Abrashkin, V.I., et al., Low-Frequency Microaccelerations onboard the Foton-11 Satellite, Kosm. Issled., 2004, vol. 42, no. 2, pp. 185–200. [Cosmic Research, pp. 194–201].
Abrashkin, V.I., Bogoyavlenskii, N.L., Voronov, K.E., et al., Uncontrolled Motion of the Foton M-2 Satellite and Quasistatic Microaccelerations on Its Board, Kosm. Issled., 2007, vol. 45, no. 5, pp. 450–470. [Cosmic Research, pp. 424–444].
Babkin, E.V., Belyaev, M.Yu., Efimov, N.I., et al., Uncontrolled Rotational Motion of the Mir Orbital Station, Kosm. Issled., 2001, vol. 39, no. 1, pp. 27–42. [Cosmic Research, pp. 23–37].
Beuselinck, T., Van Bavinchove, C., Abrashkin, V.I., et al, Determination of Foton M-3 Attitude Motion Using Onboard Measurements of the Earth’s Magnetic Field, Preprint of Keldysh Inst. of Applied Math., Russ. Acad. Sci., Moscow, 2008, no. 80.
Sazonov, V.V., Chebukov, S.Yu., Abrashkin, V.I., et al., Analysis of Low-Frequency Microaccelerations onboard the Foton-11 Satellite, Kosm. Issled., 2001, vol. 39, no. 4, pp. 419–435. [Cosmic Research, pp. 391–407].
Abrashkin, V.I., Balakin, V.L., Belokonov, I.V., et al., Uncontrolled Attitude Motion of the Foton-12 Satellite and Quasi-Steady Microaccelerations onboard It, Kosm. Issled., 2003, vol. 41, no. 1, pp. 45–56. [Cosmic Research, pp. 39–50].
Belyaev, M.Yu., Efimov, N.I., and Sazonov, V.V., Determining the Orientation of the Mir Orbital Complex Using Data of Optical Star Tracker,, Kosm. Issled., vol. 33, no. 4, pp. 395–402. [Cosmic Research, p. 357].
Author information
Authors and Affiliations
Additional information
Original Russian Text © T. Beuselinck, C. Van Bavinchove, V.I. Abrashkin, A.E. Kazakova, V.V. Sazonov, 2010, published in Kosmicheskie Issledovaniya, 2010, Vol. 48, No. 3, pp. 252–265.
Rights and permissions
About this article
Cite this article
Beuselinck, T., Van Bavinchove, C., Abrashkin, V.I. et al. Determination of attitude motion of the Foton M-3 satellite according to the data of onboard measurements of the Earth’s magnetic field. Cosmic Res 48, 246–259 (2010). https://doi.org/10.1134/S0010952510030068
Received:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0010952510030068