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Real-time quadrocopter optimal stabilization. / Popkov, Alexandr S. ; Smirnov, Nikolay V. ; Baranov, Oleg V. .

2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP). Institute of Electrical and Electronics Engineers Inc., 2015. p. 123–125 .

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

Harvard

Popkov, AS, Smirnov, NV & Baranov, OV 2015, Real-time quadrocopter optimal stabilization. in 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP). Institute of Electrical and Electronics Engineers Inc., pp. 123–125 , International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015, St. Petersburg, Russian Federation, 5/10/15. https://doi.org/10.1109/SCP.2015.7342066

APA

Popkov, A. S., Smirnov, N. V., & Baranov, O. V. (2015). Real-time quadrocopter optimal stabilization. In 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP) (pp. 123–125 ). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/SCP.2015.7342066

Vancouver

Popkov AS, Smirnov NV, Baranov OV. Real-time quadrocopter optimal stabilization. In 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP). Institute of Electrical and Electronics Engineers Inc. 2015. p. 123–125 https://doi.org/10.1109/SCP.2015.7342066

Author

Popkov, Alexandr S. ; Smirnov, Nikolay V. ; Baranov, Oleg V. . / Real-time quadrocopter optimal stabilization. 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP). Institute of Electrical and Electronics Engineers Inc., 2015. pp. 123–125

BibTeX

@inproceedings{ebfe6b7561c8464f9f2c3fc64b3b2f01,
title = "Real-time quadrocopter optimal stabilization",
abstract = "Quadrocopters (UAV with four rotors rotating diagonally in opposite directions) have a special place in UAV family. The main reasons are the possibility to easily control and maneuverability. Also quadrocopters have a low manufacturing cost and small takeoff weight. The necessity to stabilize the flight of quadrocopter follows from the principle of its operation. In this paper a system of nonlinear differential equations with control parameters that describe the flight of quadrocopter is considered. The linearization of nonlinear controlled system is constructed and description of proposals for the use of numerical method for real-time control synthesis is suggested. The possibilities of this approach are illustrated on a particular example.",
keywords = "UAV (drone), differential equations, optimal control, real-time systems",
author = "Popkov, {Alexandr S.} and Smirnov, {Nikolay V.} and Baranov, {Oleg V.}",
note = "Popkov A.S., Smirnov N.V., Baranov O.V. Real-time quadrocopter optimal stabilization // 2015 International Conference {"}Stability and Control Processes{"} in Memory of V.I. Zubov (SCP), St. Petersburg, Russia, 2015. P. 123-125.; International Conference on {"}Stability and Control Processes{"} in Memory of V.I. Zubov, SCP 2015 ; Conference date: 05-10-2015 Through 09-10-2015",
year = "2015",
doi = "10.1109/SCP.2015.7342066",
language = "English",
isbn = "978-1-4673-7698-3",
pages = "123–125 ",
booktitle = "2015 International Conference {"}Stability and Control Processes{"} in Memory of V.I. Zubov (SCP)",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
address = "United States",
url = "http://www.apmath.spbu.ru/scp2015/openconf.php",

}

RIS

TY - GEN

T1 - Real-time quadrocopter optimal stabilization

AU - Popkov, Alexandr S.

AU - Smirnov, Nikolay V.

AU - Baranov, Oleg V.

N1 - Popkov A.S., Smirnov N.V., Baranov O.V. Real-time quadrocopter optimal stabilization // 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP), St. Petersburg, Russia, 2015. P. 123-125.

PY - 2015

Y1 - 2015

N2 - Quadrocopters (UAV with four rotors rotating diagonally in opposite directions) have a special place in UAV family. The main reasons are the possibility to easily control and maneuverability. Also quadrocopters have a low manufacturing cost and small takeoff weight. The necessity to stabilize the flight of quadrocopter follows from the principle of its operation. In this paper a system of nonlinear differential equations with control parameters that describe the flight of quadrocopter is considered. The linearization of nonlinear controlled system is constructed and description of proposals for the use of numerical method for real-time control synthesis is suggested. The possibilities of this approach are illustrated on a particular example.

AB - Quadrocopters (UAV with four rotors rotating diagonally in opposite directions) have a special place in UAV family. The main reasons are the possibility to easily control and maneuverability. Also quadrocopters have a low manufacturing cost and small takeoff weight. The necessity to stabilize the flight of quadrocopter follows from the principle of its operation. In this paper a system of nonlinear differential equations with control parameters that describe the flight of quadrocopter is considered. The linearization of nonlinear controlled system is constructed and description of proposals for the use of numerical method for real-time control synthesis is suggested. The possibilities of this approach are illustrated on a particular example.

KW - UAV (drone)

KW - differential equations

KW - optimal control

KW - real-time systems

U2 - 10.1109/SCP.2015.7342066

DO - 10.1109/SCP.2015.7342066

M3 - Conference contribution

SN - 978-1-4673-7698-3

SP - 123

EP - 125

BT - 2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP)

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015

Y2 - 5 October 2015 through 9 October 2015

ER -

ID: 104001706