Standard

Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit. / Alesova, Irina; Babadzanjanz, Levon; Pototskaya, Irina; Saakyan, Artur.

Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016. ed. / V. N. Tkhai. Institute of Electrical and Electronics Engineers Inc., 2016. 7541157.

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

Harvard

Alesova, I, Babadzanjanz, L, Pototskaya, I & Saakyan, A 2016, Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit. in VN Tkhai (ed.), Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016., 7541157, Institute of Electrical and Electronics Engineers Inc., 2016 International Conference on Stability and Oscillations of Nonlinear Control Systems, STAB 2016, Moscow, Russian Federation, 1/06/16. https://doi.org/10.1109/STAB.2016.7541157

APA

Alesova, I., Babadzanjanz, L., Pototskaya, I., & Saakyan, A. (2016). Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit. In V. N. Tkhai (Ed.), Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016 [7541157] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/STAB.2016.7541157

Vancouver

Alesova I, Babadzanjanz L, Pototskaya I, Saakyan A. Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit. In Tkhai VN, editor, Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016. Institute of Electrical and Electronics Engineers Inc. 2016. 7541157 https://doi.org/10.1109/STAB.2016.7541157

Author

Alesova, Irina ; Babadzanjanz, Levon ; Pototskaya, Irina ; Saakyan, Artur. / Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit. Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016. editor / V. N. Tkhai. Institute of Electrical and Electronics Engineers Inc., 2016.

BibTeX

@inproceedings{debcfd2f05554e10bdc0335cf0912fc2,
title = "Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit",
abstract = "The active damping of the free large oscillations of a satellite on elliptical orbit is discussed. The satellite oscillations are described by non-linear differential equation of second order. According to Pontryagin's principle of maximum the fuel optimal control has piecewise constant form. Solving and fundamental matrix of the differential equation is determined with Erugin's expansion in symbolic form. The problem is reduced to the optimization task with linear quality function and two restrictions. For solving the Sequential Linear Programming method is offered. The ability of the satellite oscillations damping with fuel optimal control is demonstrated by numerical examples.",
author = "Irina Alesova and Levon Babadzanjanz and Irina Pototskaya and Artur Saakyan",
year = "2016",
month = aug,
day = "10",
doi = "10.1109/STAB.2016.7541157",
language = "English",
editor = "Tkhai, {V. N.}",
booktitle = "Proceedings of 2016 International Conference {"}Stability and Oscillations of Nonlinear Control Systems{"} (Pyatnitskiy's Conference), STAB 2016",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
address = "United States",
note = "2016 International Conference on Stability and Oscillations of Nonlinear Control Systems, STAB 2016 ; Conference date: 01-06-2016 Through 03-06-2016",

}

RIS

TY - GEN

T1 - Fuel optimal control of non-linear oscillations of a satellite on elliptical orbit

AU - Alesova, Irina

AU - Babadzanjanz, Levon

AU - Pototskaya, Irina

AU - Saakyan, Artur

PY - 2016/8/10

Y1 - 2016/8/10

N2 - The active damping of the free large oscillations of a satellite on elliptical orbit is discussed. The satellite oscillations are described by non-linear differential equation of second order. According to Pontryagin's principle of maximum the fuel optimal control has piecewise constant form. Solving and fundamental matrix of the differential equation is determined with Erugin's expansion in symbolic form. The problem is reduced to the optimization task with linear quality function and two restrictions. For solving the Sequential Linear Programming method is offered. The ability of the satellite oscillations damping with fuel optimal control is demonstrated by numerical examples.

AB - The active damping of the free large oscillations of a satellite on elliptical orbit is discussed. The satellite oscillations are described by non-linear differential equation of second order. According to Pontryagin's principle of maximum the fuel optimal control has piecewise constant form. Solving and fundamental matrix of the differential equation is determined with Erugin's expansion in symbolic form. The problem is reduced to the optimization task with linear quality function and two restrictions. For solving the Sequential Linear Programming method is offered. The ability of the satellite oscillations damping with fuel optimal control is demonstrated by numerical examples.

UR - http://www.scopus.com/inward/record.url?scp=84988369415&partnerID=8YFLogxK

U2 - 10.1109/STAB.2016.7541157

DO - 10.1109/STAB.2016.7541157

M3 - Conference contribution

AN - SCOPUS:84988369415

BT - Proceedings of 2016 International Conference "Stability and Oscillations of Nonlinear Control Systems" (Pyatnitskiy's Conference), STAB 2016

A2 - Tkhai, V. N.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 International Conference on Stability and Oscillations of Nonlinear Control Systems, STAB 2016

Y2 - 1 June 2016 through 3 June 2016

ER -

ID: 36460036