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Journal of Automation and Information Sciences
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN Imprimer: 1064-2315
ISSN En ligne: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v31.i10.150
pages 111-122

The Optimization of Atmospheric Maneuver for Mars Orbiter Insertion

A. V. Novitskiy
V. V. Zelentsov

RÉSUMÉ

The aerodynamic maneuvering for spacecraft transition from a hyperbolic trajectory onto the orbit of Mars orbiter insertion with a non-coplanar trajectory is under consideration. The objective of this studying is the expenditure decrease. For this atmospheric section we proposed the computing technique for determining the optimal control law. The numerical results are given.


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