Attitude control of a quadrotor

I. Can Dikmen; Aydemir Arisoy; Hakan Temeltaş

doi:10.1109/RAST.2009.5158286

Attitude control of a quadrotor

I. Can Dikmen, Aydemir Arisoy, Hakan Temeltaş

Department of Control and Automation Engineering

Turkish Air Force Academy

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

110 Citations (Scopus)

Abstract

This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.

Original language	English
Title of host publication	RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies
Pages	722-727
Number of pages	6
DOIs	https://doi.org/10.1109/RAST.2009.5158286
Publication status	Published - 2009
Event	4th International Conference on Recent Advances in Space Technologies 2009, RAST '09 - Istanbul, Turkey Duration: 11 Jun 2009 → 13 Jun 2009

Publication series

Name	RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies

Conference

Conference	4th International Conference on Recent Advances in Space Technologies 2009, RAST '09
Country/Territory	Turkey
City	Istanbul
Period	11/06/09 → 13/06/09

Keywords

Back stepping
Inverse dynamic control
Quadrotor
Robust control
Sliding mode

Access to Document

10.1109/RAST.2009.5158286

Cite this

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title = "Attitude control of a quadrotor",

abstract = "This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.",

keywords = "Back stepping, Inverse dynamic control, Quadrotor, Robust control, Sliding mode",

author = "Dikmen, \{I. Can\} and Aydemir Arisoy and Hakan Temelta{\c s}",

year = "2009",

doi = "10.1109/RAST.2009.5158286",

language = "English",

isbn = "9781424436286",

series = "RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies",

pages = "722--727",

booktitle = "RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies",

note = "4th International Conference on Recent Advances in Space Technologies 2009, RAST '09 ; Conference date: 11-06-2009 Through 13-06-2009",

}

Dikmen, IC, Arisoy, A & Temeltaş, H 2009, Attitude control of a quadrotor. in RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies., 5158286, RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies, pp. 722-727, 4th International Conference on Recent Advances in Space Technologies 2009, RAST '09, Istanbul, Turkey, 11/06/09. https://doi.org/10.1109/RAST.2009.5158286

Attitude control of a quadrotor. / Dikmen, I. Can; Arisoy, Aydemir; Temeltaş, Hakan.
RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies. 2009. p. 722-727 5158286 (RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies).

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

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AU - Dikmen, I. Can

AU - Arisoy, Aydemir

AU - Temeltaş, Hakan

PY - 2009

Y1 - 2009

N2 - This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.

AB - This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.

KW - Back stepping

KW - Inverse dynamic control

KW - Quadrotor

KW - Robust control

KW - Sliding mode

UR - https://www.scopus.com/pages/publications/70350431760

U2 - 10.1109/RAST.2009.5158286

DO - 10.1109/RAST.2009.5158286

M3 - Conference contribution

AN - SCOPUS:70350431760

SN - 9781424436286

T3 - RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies

SP - 722

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BT - RAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies

T2 - 4th International Conference on Recent Advances in Space Technologies 2009, RAST '09

Y2 - 11 June 2009 through 13 June 2009

ER -

Attitude control of a quadrotor

Abstract

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Keywords

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