Fuel/Time optimal control of satellite oscillations

Standard

Fuel/Time optimal control of satellite oscillations. / Alesova, Irina M.; Babadzanjanz, Levon K.; Pototskaya, Irina Yu ; Pupysheva, Yulia Yu ; Saakyan, Artur T.

International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016. ed. / Theodore E. Simos; Theodore E. Simos; Charalambos Tsitouras. American Institute of Physics, 2017. 170008 (AIP Conference Proceedings; Vol. 1863).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Harvard

Alesova, IM , Babadzanjanz, LK , Pototskaya, IY , Pupysheva, YY & Saakyan, AT 2017, Fuel/Time optimal control of satellite oscillations. in TE Simos, TE Simos & C Tsitouras (eds), International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016., 170008, AIP Conference Proceedings, vol. 1863, American Institute of Physics, International Conference of Numerical Analysis and Applied Mathematics 2016, ICNAAM 2016, Rhodes, Greece, 19/09/16. https://doi.org/10.1063/1.4992353

APA

Alesova, I. M., Babadzanjanz, L. K., Pototskaya, I. Y., Pupysheva, Y. Y., & Saakyan, A. T. (2017). Fuel/Time optimal control of satellite oscillations. In T. E. Simos, T. E. Simos, & C. Tsitouras (Eds.), International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016 [170008] (AIP Conference Proceedings; Vol. 1863). American Institute of Physics. https://doi.org/10.1063/1.4992353

Vancouver

Alesova IM , Babadzanjanz LK , Pototskaya IY , Pupysheva YY , Saakyan AT. Fuel/Time optimal control of satellite oscillations. In Simos TE, Simos TE, Tsitouras C, editors, International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016. American Institute of Physics. 2017. 170008. (AIP Conference Proceedings). https://doi.org/10.1063/1.4992353

Author

Alesova, Irina M. ; Babadzanjanz, Levon K. ; Pototskaya, Irina Yu ; Pupysheva, Yulia Yu ; Saakyan, Artur T. / Fuel/Time optimal control of satellite oscillations. International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016. editor / Theodore E. Simos ; Theodore E. Simos ; Charalambos Tsitouras. American Institute of Physics, 2017. (AIP Conference Proceedings).

BibTeX

@inproceedings{1738a545ba494f74a5e03837619d2a60,

title = "Fuel/Time optimal control of satellite oscillations",

abstract = "In this paper the analysis of the fuel/time optimal control of the plane oscillations of the satellite on the elliptical orbit has been done. The numerical method of the sequential linearization of the boundary conditions for the optimal calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states and the different time-optimal values of hybridization coefficient γ have been calculated.",

author = "Alesova, {Irina M.} and Babadzanjanz, {Levon K.} and Pototskaya, {Irina Yu} and Pupysheva, {Yulia Yu} and Saakyan, {Artur T.}",

note = "Publisher Copyright: {\textcopyright} 2017 Author(s). Copyright: Copyright 2017 Elsevier B.V., All rights reserved.; International Conference of Numerical Analysis and Applied Mathematics 2016, ICNAAM 2016, ICNAAM 2016 ; Conference date: 19-09-2016 Through 25-09-2016",

year = "2017",

month = jul,

day = "21",

doi = "10.1063/1.4992353",

language = "English",

series = "AIP Conference Proceedings",

publisher = "American Institute of Physics",

editor = "Simos, {Theodore E.} and Simos, {Theodore E.} and Charalambos Tsitouras",

booktitle = "International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016",

address = "United States",

url = "http://icnaam.org/",

}

RIS

TY - GEN

T1 - Fuel/Time optimal control of satellite oscillations

AU - Alesova, Irina M.

AU - Babadzanjanz, Levon K.

AU - Pototskaya, Irina Yu

AU - Pupysheva, Yulia Yu

AU - Saakyan, Artur T.

PY - 2017/7/21

Y1 - 2017/7/21

N2 - In this paper the analysis of the fuel/time optimal control of the plane oscillations of the satellite on the elliptical orbit has been done. The numerical method of the sequential linearization of the boundary conditions for the optimal calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states and the different time-optimal values of hybridization coefficient γ have been calculated.

AB - In this paper the analysis of the fuel/time optimal control of the plane oscillations of the satellite on the elliptical orbit has been done. The numerical method of the sequential linearization of the boundary conditions for the optimal calculation of the switching moments has been proposed and its implementation has been presented. Examples for the different areas of the initial states and the different time-optimal values of hybridization coefficient γ have been calculated.

UR - http://www.scopus.com/inward/record.url?scp=85026633717&partnerID=8YFLogxK

U2 - 10.1063/1.4992353

DO - 10.1063/1.4992353

M3 - Conference contribution

AN - SCOPUS:85026633717

T3 - AIP Conference Proceedings

BT - International Conference of Numerical Analysis and Applied Mathematics, ICNAAM 2016

A2 - Simos, Theodore E.

A2 - Tsitouras, Charalambos

PB - American Institute of Physics

T2 - International Conference of Numerical Analysis and Applied Mathematics 2016, ICNAAM 2016

Y2 - 19 September 2016 through 25 September 2016

ER -

ID: 73212913