Terminal synthesis of orbital orientation for a spacecraft-Reference-Cited by-同舟云学术

Terminal synthesis of orbital orientation for a spacecraft

Published:2017-07 Issue:4 Volume:56 Page:721-737
ISSN:1064-2307
Container-title:Journal of Computer and Systems Sciences International
language:en
Short-container-title:J. Comput. Syst. Sci. Int.

Author:

Zubov N. E.,Li M. V.,Mikrin E. A.,Ryabchenko V. N.

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

http://link.springer.com/content/pdf/10.1134/S1064230717040190.pdf

Reference17 articles.

1. N. E. Zubov, “Algorithmic support of automatic mode of spacecraft orbital orientation,” Izv. Akad. Nauk SSSR, Tekh. Kibernet., No. 2, 193–202 (1990).

2. N. E. Zubov, “Optimal control of spacecraft terminal reorientation based on algorithm with forecasting model,” Kosm. Issled. 29, 340–350 (1991).

3. Reference Book on Automatic Control, Ed. by A. A. Krasovskii (Nauka, Moscow, 1987) [in Russian].

4. E. A. Mikrin, N. E. Zubov, S. S. Negodyaev, et al., “Optimal control of spacecraft orbital orientation based on algorithm with forecasting model,” Tr. MFTI 2, 189–195 (2010).

5. N. E. Zubov, E. A. Mikrin, M. Sh. Misrikhanov, V. N. Ryabchenko, S. N. Timakov, and E. A. Cheremnykh, “Identification of the position of an equilibrium attitude of the international space station as a problem of stable matrix completion,” J. Comput. Syst. Sci. Int. 51, 291 (2012).

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Optimal Control of the Reorientation of a Spacecraft in the Given Time with a Quadratic Performance Criterion Related to the Control and Phase Variables;Journal of Computer and Systems Sciences International;2023-06

2. Optimal Control of the Angular Momentum for a Solid (Spacecraft) Performing a Spatial Turn;Mechanics of Solids;2023-02

3. Stabilizing the orbital orientation of a spacecraft at the absence of angles measurements;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

4. Optimal Orientation Control of a Space Vehicle with Restrictions on the Control and Phase Variables;Journal of Computer and Systems Sciences International;2021-11

5. Usage of a Combined Criterion of Quality in the Dynamic Problem on Optimal Rotation of a Solid (Spacecraft) with a Constraint Imposed on the Phase Variables;Mechanics of Solids;2021-09