Magnetic stabilization of a spacecraft and the effect of compensation of information errors-Reference-Cited by-同舟云学术

Magnetic stabilization of a spacecraft and the effect of compensation of information errors

Published:2012-02 Issue:1 Volume:50 Page:76-85
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Tkachenko A. I.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952512010108.pdf

Reference13 articles.

1. Psiaki, M.L., Martel, F., and Pal, P.K., Three-Axis Attitude Determination via Kalman Filtering of Magnetometer Data, J. Guidance, Control, and Dynamics, 1990, vol. 13, no. 3.

2. Lebedev, D.V. and Tkachenko, A.I., Control over Spherical Motion of a Spacecraft in the Earth’s Magnetic Field. Part II: Orientation and Stabilization, Probl. Upravlen. Inform., 1996, no. 3.

3. Efimenko, N.V., Magnetic System of Orientation and Stabilization for the EgyptSat-1 Spacecraft, Probl. Upravlen. i Inform., 2010, no. 6.

4. Lebedev, D.V., Stabilization of Motion for One Class of Nonlinear Systems, Probl. Upravlen. i Inform., 2002, no. 1.

5. Branets, V.N. and Shmyglevskii, I.P., Primenenie kvaternionov v zadachakh orientatsii tverdogo tela (Application of Quaternions in Problems of Orientation of Solid Bodies), Moscow: Nauka, 1973.

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