Geodesic
On the method of synthesis of optimal control of spacecraft reorientation during sensing hardware redirection
Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 9 (2013), pp. 208-214

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The problem of optimal control of spacecraft reorientation during remote earth sensing hardware redirection is considered. Computational algorithm for the approximate solution of the problem is developed. Efficiency of this algorithm is confirmed by the results of the performed modeling.
Keywords: spacecraft, remote Earth sensing, angular motion, optimal control, algorithms.
Mots-clés : redirection 
@article{VSGU_2013_9_a23,
     author = {M. V. Morozova},
     title = {On the method of synthesis of optimal control of spacecraft reorientation during sensing hardware redirection},
     journal = {Vestnik Samarskogo universiteta. Estestvennonau\v{c}na\^a seri\^a},
     pages = {208--214},
     publisher = {mathdoc},
     number = {9},
     year = {2013},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VSGU_2013_9_a23/}
}
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M. V. Morozova. On the method of synthesis of optimal control of spacecraft reorientation during sensing hardware redirection. Vestnik Samarskogo universiteta. Estestvennonaučnaâ seriâ, no. 9 (2013), pp. 208-214. http://geodesic.mathdoc.fr/item/VSGU_2013_9_a23/