Motion of a descent capsule relative to its center of mass when deploying the orbital tether system
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Beletskii, V.V. and Levin, E.M., Dinamika kosmicheskikh trosovykh sistem (Dynamics of Space Tether Systems), Moscow: Nauka, 1990.
Alpatov, A.P. Beletskii, V.V., et al., Dinamika kosmicheskikh sistem s trosovymi i sharnirnymi soedineniyami (Dynamics of Space Systems with Tether and Hinge Connections), Moscow-Izhevsk: Research Center “Regular and Chaotic Dynamics” and Institute for Computer Studies, 2007.
Ivanov, V.A. and Sitarskii, Yu.S., Dinamika poleta sistemy gibko svyazannykh kosmicheskikh ob″ektov (Flight Dynamics of a System of Flexibly Connected Space Objects), Moscow: Mashinostroenie, 1986.
Kruijff, M., Heide, E., Stelzer, M., et al., First Mission Results of the YES2 Tethered Space Mail Experiment, AIAA-2008-7385.
Menon, C., Kruijff, M., and Vavonliotis, A., Design and Testing of a Space Mechanism for Tether Deployment, J. Spacecr. Rockets, 2007, vol. 44, no. 4.
Zabolotnova, O.Yu., Choosing a Criterion when Solving the Problem of Regulation of Deployment of a Space Tethered System, Internet Journal “Investigated in Russia”, 2007-070; http://zhurnal.ape.relarn.ru/articles/2007/070.pdf
Williams, P., Hyslop, A., and Kruijff, M., Deployment Control for the YES2 Tether-Assisted Re-Entry Mission, Advances in the Astronautical Sciences, 2006, vol. 123, pp. 1101–1120.
Zabolotnov, Yu.M. and Fefelov, D.I., Dynamics of Motion of a Capsule with Tether on the Extra-Atmospheric Segment of Its Descent Trajectory, Izv. of Samara Research Center of Ross. Akad. Nauk, 2006, vol. 8, no. 3, pp. 841–848.
Zabolotnov, Yu.M., Asymptotic Analysis of Quasilinear Equations of Motion of a Spacecraft with Small Asymmetry in the Atmosphere: I., Kosm. Issled., 1993, vol. 31, no. 6, pp. 39–50. [Cosmic Research, p. 620].
Landau, L.D. and Lifshits, E.M., Teoreticheskaya fizika: T. 1. Mekhanika (Theoretical Physics: vol. 1, Mechanics), Moscow: Nauka, 1988.
Ishkov, S.A. and Naumov, S.A., Control over Deployment of an Orbital Tethered System, Vestnik Samarskogo Gos. Aerokosm. Univ., 2006, no. 1, pp. 81–90.
Zabolotnov, Yu.M., Asymptotic Analysis of Quasilinear Equations of Motion of a Spacecraft with Small Asymmetry in the Atmosphere: III., Kosm. Issled., 1994, vol. 32, nos. 4–5, pp. 112–125. [Cosmic Research, p. 447].
Zabolotnov, Yu.M. and Lyubimov, V.V., Application of the Method of Integral Manifolds for Construction of Resonant Curves for the Problem of Spacecraft Entry into the Atmosphere, Kosm. Issled., 2003, vol. 41, no. 5, pp. 481–487. [Cosmic Research, pp. 453–459].