Nonlinear Stochastic Evaluation of the Orientation Parameters of a Strapdown Inertial Navigation System of a Space Vehicle During Prelaunch Preparation-Reference-Cited by-同舟云学术

Nonlinear Stochastic Evaluation of the Orientation Parameters of a Strapdown Inertial Navigation System of a Space Vehicle During Prelaunch Preparation

Published:2021-11 Issue:6 Volume:60 Page:1005-1015
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Gashenenko I. N.,Pogorelov V. A.,Sokolov S. V.,Shatalov A. B.

Publisher

Pleiades Publishing Ltd

Subject

Applied Mathematics,Computer Networks and Communications,Computer Vision and Pattern Recognition,Information Systems,Theoretical Computer Science,Control and Systems Engineering,Software

Link

https://link.springer.com/content/pdf/10.1134/S1064230721060083.pdf

Reference31 articles.

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2. L. N. Lysenko, V. V. Betanov, and F. V. Zvyagin, Theoretical Foundations of Ballistic and Navigation Support of Space Flights (MGTU, Moscow, 2014) [in Russian].

3. V. K. Serdyuk, Design of Spacecraft Launch Vehicles (Mashinostroenie, Moscow, 2009) [in Russian].

4. N. M. Ivanov and L. N. Lysenko, Ballistics and Spacecraft Navigation (Drofa, Moscow, 2004) [in Russian].

5. N. Yu. Borisenko and A. V. Sumarokov, “On the rapid orbital attitude control of manned and cargo spacecraft Soyuz MS and Progress MS,” J. Comput. Syst. Sci. Int. 56, 886 (2017).

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