Geodesic
On an optimal orbit transfer in a normal gravitational field
Trudy Instituta matematiki i mehaniki, Trudy Instituta Matematiki i Mekhaniki UrO RAN, Tome 21 (2015) no. 3, pp. 142-152 Cet article a éte moissonné depuis la source Math-Net.Ru

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We consider an optimal control problem for a nonlinear dynamic system describing the motion of a special-purpose spacecraft in a normal gravitational field. The spacecraft is designed for transporting a payload from a near-Earth elliptic orbit to a higher target orbit. The required control must satisfy a number of constraints and provide the transfer of a maximum-weight payload to a given target orbit under some requirements on the current phase state of the system. We propose approaches to the solution of this problem and present results of numerical simulation.
Mots-clés : orbit transfer
Keywords: optimal control, finite thrust, payload, state constraints. 
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I. N. Kandoba; I. V. Koz'min; V. B. Kostousov; E. K. Kostousova; A. B. Lozhnikov; V. I. Pochinskii. On an optimal orbit transfer in a normal gravitational field. Trudy Instituta matematiki i mehaniki, Trudy Instituta Matematiki i Mekhaniki UrO RAN, Tome 21 (2015) no. 3, pp. 142-152. http://geodesic.mathdoc.fr/item/TIMM_2015_21_3_a15/

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