Construction of the initial deorbit region for landing at the given place

S. N. Evdokimov; S. I. Klimanov; A. N. Korchagin; E. A. Mikrin; Yu. G. Sikharulidze; A. G. Tuchin

doi:10.1134/S106423071702006X

Construction of the initial deorbit region for landing at the given place

Authors: Evdokimov S.N.¹^,2, Klimanov S.I.¹^,2, Korchagin A.N.¹^,2, Mikrin E.A.¹^,2, Sikharulidze Y.G.¹^,2, Tuchin A.G.¹^,2
Affiliations:
1. Keldysh Institute of Applied Mathematics
2. Korolev Rocket and Space Corporation Energia
Issue: Vol 56, No 2 (2017)
Pages: 300-310
Section: Control Systems of Moving Objects
URL: https://journals.rcsi.science/1064-2307/article/view/219861
DOI: https://doi.org/10.1134/S106423071702006X
ID: 219861

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Abstract

The algorithm of the two-point boundary problem is developed for choice the nominal deorbit point, from which a descent vehicle is enabled to land at a given place without a cross-range maneuver. The method is suggested and the example is given of constructing the initial deorbit region for landing at the Vostochny cosmodrome.