Standard

Control of satellite aerodynamic oscillations. / Alesova, I. M.; Babadzanjanz, L. K.; Bregman, A. M.; Bregman, K. M.; Pototskaya, I. Yu; Pupysheva, Yu Yu; Saakyan, A. T.

International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017. ed. / Charalambos Tsitouras; Theodore Simos. American Institute of Physics, 2018. 100007 (AIP Conference Proceedings; Vol. 1978).

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Harvard

Alesova, IM, Babadzanjanz, LK, Bregman, AM, Bregman, KM, Pototskaya, IY, Pupysheva, YY & Saakyan, AT 2018, Control of satellite aerodynamic oscillations. in C Tsitouras & T Simos (eds), International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017., 100007, AIP Conference Proceedings, vol. 1978, American Institute of Physics, 15th International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017, Thessaloniki, Greece, 25/09/17. https://doi.org/10.1063/1.5043751

APA

Alesova, I. M., Babadzanjanz, L. K., Bregman, A. M., Bregman, K. M., Pototskaya, I. Y., Pupysheva, Y. Y., & Saakyan, A. T. (2018). Control of satellite aerodynamic oscillations. In C. Tsitouras, & T. Simos (Eds.), International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017 [100007] (AIP Conference Proceedings; Vol. 1978). American Institute of Physics. https://doi.org/10.1063/1.5043751

Vancouver

Alesova IM, Babadzanjanz LK, Bregman AM, Bregman KM, Pototskaya IY, Pupysheva YY et al. Control of satellite aerodynamic oscillations. In Tsitouras C, Simos T, editors, International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017. American Institute of Physics. 2018. 100007. (AIP Conference Proceedings). https://doi.org/10.1063/1.5043751

Author

Alesova, I. M. ; Babadzanjanz, L. K. ; Bregman, A. M. ; Bregman, K. M. ; Pototskaya, I. Yu ; Pupysheva, Yu Yu ; Saakyan, A. T. / Control of satellite aerodynamic oscillations. International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017. editor / Charalambos Tsitouras ; Theodore Simos. American Institute of Physics, 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{f22657cd9f664b1296667c5e9c8e2e4d,
title = "Control of satellite aerodynamic oscillations",
abstract = "In this paper the analysis of the fuel optimal control of the plane oscillations of the satellite on the circular orbit subject to the aerodynamic moment variations has been done. On basis of necessary conditions of optimality the problem was reduced to the task of nonlinear programming. The numerical method of the sequential linearization of the boundary conditions for calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states have been calculated.",
author = "Alesova, {I. M.} and Babadzanjanz, {L. K.} and Bregman, {A. M.} and Bregman, {K. M.} and Pototskaya, {I. Yu} and Pupysheva, {Yu Yu} and Saakyan, {A. T.}",
note = "Funding Information: The authors acknowledge Saint-Petersburg State University for a research grant 9.37.345.2015. Publisher Copyright: {\textcopyright} 2018 Author(s). Copyright: Copyright 2018 Elsevier B.V., All rights reserved.; 15th International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017 ; Conference date: 25-09-2017 Through 30-09-2017",
year = "2018",
month = jul,
day = "10",
doi = "10.1063/1.5043751",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics",
editor = "Charalambos Tsitouras and Theodore Simos",
booktitle = "International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017",
address = "United States",

}

RIS

TY - GEN

T1 - Control of satellite aerodynamic oscillations

AU - Alesova, I. M.

AU - Babadzanjanz, L. K.

AU - Bregman, A. M.

AU - Bregman, K. M.

AU - Pototskaya, I. Yu

AU - Pupysheva, Yu Yu

AU - Saakyan, A. T.

N1 - Funding Information: The authors acknowledge Saint-Petersburg State University for a research grant 9.37.345.2015. Publisher Copyright: © 2018 Author(s). Copyright: Copyright 2018 Elsevier B.V., All rights reserved.

PY - 2018/7/10

Y1 - 2018/7/10

N2 - In this paper the analysis of the fuel optimal control of the plane oscillations of the satellite on the circular orbit subject to the aerodynamic moment variations has been done. On basis of necessary conditions of optimality the problem was reduced to the task of nonlinear programming. The numerical method of the sequential linearization of the boundary conditions for calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states have been calculated.

AB - In this paper the analysis of the fuel optimal control of the plane oscillations of the satellite on the circular orbit subject to the aerodynamic moment variations has been done. On basis of necessary conditions of optimality the problem was reduced to the task of nonlinear programming. The numerical method of the sequential linearization of the boundary conditions for calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states have been calculated.

UR - http://www.scopus.com/inward/record.url?scp=85049981997&partnerID=8YFLogxK

U2 - 10.1063/1.5043751

DO - 10.1063/1.5043751

M3 - Conference contribution

AN - SCOPUS:85049981997

T3 - AIP Conference Proceedings

BT - International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017

A2 - Tsitouras, Charalambos

A2 - Simos, Theodore

PB - American Institute of Physics

T2 - 15th International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2017

Y2 - 25 September 2017 through 30 September 2017

ER -

ID: 73213801