Resonance Effects when Moving a Small Spacecraft around the Center of Mass in a Deployable Tether System

Author:

Zabolotnov Yu. M.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Reference21 articles.

1. Alpatov, A.P., Beletskii, V.V., Dranovskii, V.I., et al., Dinamika kosmicheskikh sistem s trosovymi i sharnirnymi soedineniyami (Dynamics of Tethered and Jointed Space Systems), Moscow–Izhevsk: Regulyarnaya i khaoticheskaya dinamika, Inst. Komp. Issled., 2007.

2. Beletskii, V.V. and Levin, E.M., Dinamika kosmicheskikh trosovykh sistem (Dynamics of Tethered Space Systems), Moscow: Nauka, 1990.

3. Zabolotnov, Yu.M., Resonant motions of a statically stable Lagrange top at small nutation angles, Prikl. Mat. Mekh., 2016, vol. 80, no. 4, pp. 432–443.

4. Zabolotnov, Yu.M., Resonant motions of a statically stable Lagrange top, Prikl. Mat. Mekh., 2019, vol. 83, no. 4, pp. 615–635.

5. Zabolotnov, Yu.M. and Naumov, O.N., Motion of a descent capsule relative to its center of mass when deploying the orbital tether system, Cosmic Res., 2012, vol. 50, no. 2, pp. 177–187.

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