On a problem of optimal putting a payload into a given elliptic orbit
Trudy Instituta matematiki i mehaniki, Trudy Instituta Matematiki i Mekhaniki UrO RAN, Tome 16 (2010) no. 5, pp. 57-65
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A problem of optimal open-loop control for a carrier rocket of “Soyuz” type is considered. The aim is to put maximal payloads into given low earth elliptic orbits.
Keywords: optimal control, maximum payload, osculating orbit, numerical methods.
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T. D. Dumsheva; V. B. Kostousov; E. K. Kostousova; V. I. Potchinskii. On a problem of optimal putting a payload into a given elliptic orbit. Trudy Instituta matematiki i mehaniki, Trudy Instituta Matematiki i Mekhaniki UrO RAN, Tome 16 (2010) no. 5, pp. 57-65. http://geodesic.mathdoc.fr/item/TIMM_2010_16_5_a7/

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