2022
DOI: 10.1007/s11044-022-09845-w
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Development and verification of a flexible tethered satellite system model considering the fuel slosh

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Cited by 5 publications
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“…Usually, it consists of the mother satellite of mass m 1 moving in an unperturbed Kepler circular orbit and the sub-satellite of mass m 2 attached to the mother satellite through an elastic massless tether of length l(t). Although active debris removal using a tethered tug-debris system is a relatively new topic, several books [88][89][90] and hundreds of scientific articles have been already published [90][91][92][93]. However, many aspects of this problem remain unexplored.…”
Section: Theorem 11 (Morales-ramis (1999)) If a Hamiltonian System Is...mentioning
confidence: 99%
“…Usually, it consists of the mother satellite of mass m 1 moving in an unperturbed Kepler circular orbit and the sub-satellite of mass m 2 attached to the mother satellite through an elastic massless tether of length l(t). Although active debris removal using a tethered tug-debris system is a relatively new topic, several books [88][89][90] and hundreds of scientific articles have been already published [90][91][92][93]. However, many aspects of this problem remain unexplored.…”
Section: Theorem 11 (Morales-ramis (1999)) If a Hamiltonian System Is...mentioning
confidence: 99%