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Stability of a tethered satellite subjected to stochastic forces
Acta Astronautica, 1991Abstract This paper considers the problem of the relative equilibrium and stability of a tethered subsatellite (TSS), when the aerodynamic forces can be only probabilistically evaluated. The location in the space of the TSS is thus a stochastic process. The range of possible stationary states of the system is determined and a procedure is adopted for
DE MATTEIS, GUIDO, DE SOCIO, Luciano
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Quadrature discretization method in tethered satellite control
Applied Mathematics and Computation, 2011zbMATH Open Web Interface contents unavailable due to conflicting licenses.
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Periodic motion in the tethered satellite system
Journal of Guidance, Control, and Dynamics, 1996The tethered satellite system (TSS) operating in an elliptic orbit may have a periodic motion. The configuration and stability of the limit cycle depend on the control algorithm and the orbital eccentricity. The size of the limit cycle increases as the orbital eccentricity increases.
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Orbit-attitude-vibration coupled dynamics of tethered solar power satellite
Advances in Space Research, 2021Yi Wei, Qingjun Li
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Spin deployment of Hub-Spoke tethered satellite formation with sliding mode tether tension control
Advances in Space Research, 2023Junjie Kang, Zheng H Zhu
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Dynamic analysis of a tethered satellite system for space debris capture
Nonlinear Dynamics, 2018Jintai Chung, Chung Jintai
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Dynamics of a tethered satellite formation for space exploration modeled via ANCF
Acta Astronautica, 2020Caoqun Luo
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Dynamics of tethered satellite systems
2012Vladimir S. Aslanov, Alexander S. Ledkov
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