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Stabilization of PVTOL aircraft by supertwisting algorithms. / Popov, Alexander; Andrievsky, Boris; Zaitceva, Iuliia.

2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015. Institute of Electrical and Electronics Engineers Inc., 2015. 7154645 (2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015).

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

Harvard

Popov, A, Andrievsky, B & Zaitceva, I 2015, Stabilization of PVTOL aircraft by supertwisting algorithms. in 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015., 7154645, 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015, Institute of Electrical and Electronics Engineers Inc., International Workshop on Recent Advances in Sliding Modes, RASM 2015, Istanbul, Turkey, 9/04/15. https://doi.org/10.1109/RASM.2015.7154645

APA

Popov, A., Andrievsky, B., & Zaitceva, I. (2015). Stabilization of PVTOL aircraft by supertwisting algorithms. In 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015 [7154645] (2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RASM.2015.7154645

Vancouver

Popov A, Andrievsky B, Zaitceva I. Stabilization of PVTOL aircraft by supertwisting algorithms. In 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015. Institute of Electrical and Electronics Engineers Inc. 2015. 7154645. (2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015). https://doi.org/10.1109/RASM.2015.7154645

Author

Popov, Alexander ; Andrievsky, Boris ; Zaitceva, Iuliia. / Stabilization of PVTOL aircraft by supertwisting algorithms. 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015. Institute of Electrical and Electronics Engineers Inc., 2015. (2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015).

BibTeX

@inproceedings{d928111e04354ae6ad9c216dd07f08ed,
title = "Stabilization of PVTOL aircraft by supertwisting algorithms",
abstract = "The paper is devoted to application of sliding mode control technique for stabilization of a planar vertical takeoff and landing aircraft. Lateral motion of the autonomous aircraft is considered, containing two planar coordinates of the aircraft center of gravity and one angular coordinate for aircraft attitude. To verify the theoretical statements, simulations in Matlab/Simulink environment have been carried out. The cases of varying degrees of the control channels interference, parametric perturbations, external disturbances as the sums of harmonic signals, and unmodeled dynamics have been studied by a simulation. The case of aircraft control without output signals derivatives measurement was examined. For differentiation, the super-twisting algorithms have been employed. The results obtained show a good system performance.",
keywords = "PVTOL aircraft, Sliding mode, Super-twisting algorithm, Unmodeled dynamics",
author = "Alexander Popov and Boris Andrievsky and Iuliia Zaitceva",
year = "2015",
month = jan,
day = "1",
doi = "10.1109/RASM.2015.7154645",
language = "English",
series = "2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
booktitle = "2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015",
address = "United States",
note = "International Workshop on Recent Advances in Sliding Modes, RASM 2015 ; Conference date: 09-04-2015 Through 11-04-2015",

}

RIS

TY - GEN

T1 - Stabilization of PVTOL aircraft by supertwisting algorithms

AU - Popov, Alexander

AU - Andrievsky, Boris

AU - Zaitceva, Iuliia

PY - 2015/1/1

Y1 - 2015/1/1

N2 - The paper is devoted to application of sliding mode control technique for stabilization of a planar vertical takeoff and landing aircraft. Lateral motion of the autonomous aircraft is considered, containing two planar coordinates of the aircraft center of gravity and one angular coordinate for aircraft attitude. To verify the theoretical statements, simulations in Matlab/Simulink environment have been carried out. The cases of varying degrees of the control channels interference, parametric perturbations, external disturbances as the sums of harmonic signals, and unmodeled dynamics have been studied by a simulation. The case of aircraft control without output signals derivatives measurement was examined. For differentiation, the super-twisting algorithms have been employed. The results obtained show a good system performance.

AB - The paper is devoted to application of sliding mode control technique for stabilization of a planar vertical takeoff and landing aircraft. Lateral motion of the autonomous aircraft is considered, containing two planar coordinates of the aircraft center of gravity and one angular coordinate for aircraft attitude. To verify the theoretical statements, simulations in Matlab/Simulink environment have been carried out. The cases of varying degrees of the control channels interference, parametric perturbations, external disturbances as the sums of harmonic signals, and unmodeled dynamics have been studied by a simulation. The case of aircraft control without output signals derivatives measurement was examined. For differentiation, the super-twisting algorithms have been employed. The results obtained show a good system performance.

KW - PVTOL aircraft

KW - Sliding mode

KW - Super-twisting algorithm

KW - Unmodeled dynamics

UR - http://www.scopus.com/inward/record.url?scp=84964089142&partnerID=8YFLogxK

U2 - 10.1109/RASM.2015.7154645

DO - 10.1109/RASM.2015.7154645

M3 - Conference contribution

AN - SCOPUS:84964089142

T3 - 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015

BT - 2015 International Workshop on Recent Advances in Sliding Modes, RASM 2015

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - International Workshop on Recent Advances in Sliding Modes, RASM 2015

Y2 - 9 April 2015 through 11 April 2015

ER -

ID: 41251720