Geodesic
Mathematical model of space tether system in form of the Hamilton equations
Matematičeskoe modelirovanie, Tome 27 (2015) no. 9, pp. 65-72

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The space tether system is considered here, this system consists of a base spacecraft, descent capsule and elastic tether. The equations of motion of the system in the Hamiltonian form are presented in this paper. The analysis of the process of managed deployment rope on board of the spacecraft is given. The present mathematical model can be used for design calculations in the dynamics of space tethered systems.
Keywords: space tether system, Hamilton's equations, generalized coordinates, generalized momentum. 
@article{MM_2015_27_9_a4,
     author = {O. N. Naumov},
     title = {Mathematical model of space tether system in form of the {Hamilton} equations},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {65--72},
     publisher = {mathdoc},
     volume = {27},
     number = {9},
     year = {2015},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2015_27_9_a4/}
}
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O. N. Naumov. Mathematical model of space tether system in form of the Hamilton equations. Matematičeskoe modelirovanie, Tome 27 (2015) no. 9, pp. 65-72. http://geodesic.mathdoc.fr/item/MM_2015_27_9_a4/