Geodesic
Method of the accelerated calculation of spacecraft motion in the atmosphere with attached tether aerodynamic stabilizer
Matematičeskoe modelirovanie, Tome 25 (2013) no. 7, pp. 37-47

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The method of the accelerated calculation of spacecraft motion in the atmosphere with attached tether aerodynamic stabilizer is considered. Method is based on artificial increase of the oscillation periods. The method allows reducing complexity of calculations in tens of times and allows reducing influence of a computing error on accuracy of numerical integration. The algorithm for aprioristic choice of the magnification factor of oscillation periods is offered.
Keywords: artificial increase of the oscillation periods, accelerated calculation, spacecraft, tether system, aerodynamic stabilizer. 
@article{MM_2013_25_7_a2,
     author = {Yu. M. Zabolotnov and D. V. Elenev},
     title = {Method of the accelerated calculation of spacecraft motion in the atmosphere with attached tether aerodynamic stabilizer},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {37--47},
     publisher = {mathdoc},
     volume = {25},
     number = {7},
     year = {2013},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2013_25_7_a2/}
}
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Yu. M. Zabolotnov; D. V. Elenev. Method of the accelerated calculation of spacecraft motion in the atmosphere with attached tether aerodynamic stabilizer. Matematičeskoe modelirovanie, Tome 25 (2013) no. 7, pp. 37-47. http://geodesic.mathdoc.fr/item/MM_2013_25_7_a2/