Symbolic-Analytic Methods for Studying Equilibrium Orientations of a Satellite on a Circular Orbit

Author:

Gutnik S. A.,Sarychev V. A.

Publisher

Pleiades Publishing Ltd

Subject

Software

Reference22 articles.

1. Sarychev, V.A., Asymptotically stable stationary rotational motions of a satellite, Proc. 1st IFAC Symp. Automatic Control in Space, 1966, pp. 277–286.

2. Likins, P.W. and Roberson, R.E., Uniqueness of equilibrium attitudes for earth-pointing satellites, J. Astronaut Sci., 1966, vol. 13, no. 2, pp. 87–88.

3. Beletskii, V.V., Dvizhenie sputnika otnositel’no tsentra mass v gravitatsionnom pole (Satellite Motion Relative to the Center of Mass in a Gravitational Field), Moscow: Izd. Mos. Univ., 1975.

4. Sarychev, V.A., Orientation issues of artificial satellites, Itogi Nauki Tekh., Ser.: Issled. Kosm. Prostranstva, 1978, vol. 11.

5. Gutnik, S.A., Santush, L., Sarychev, V.A., and Silva, A., Dynamics of a gyrostat satellite under the action of the gravitational moment: Equilibrium positions and their stability, Izv. Akad. Nauk, Teor. Sist. Upr., 2015, no. 3, pp. 142–155.

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