Realization of the flight control for an indoor UAV quadrotor

Yi Rui Tang; Yangmin Li

doi:10.1109/ICInfA.2013.6720491

Realization of the flight control for an indoor UAV quadrotor

Research output: Chapter in book / Conference proceeding › Conference article published in proceeding or book › Academic research › peer-review

10 Citations (Scopus)

Abstract

The UAV quadrotor is considerably difficult to be controlled due to its inherently unstable and complex multi-variable properties. To realize the control, a nonlinear dynamic model is firstly derived and formulated. A control approach employing hierarchical multiple-layer structure is then developed. The detailed hardware components, software as well as the working principle of the system are described. The entire UAV control system is tested and verified in actual flight tests.

Original language	English
Title of host publication	2013 IEEE International Conference on Information and Automation, ICIA 2013
Pages	1278-1283
Number of pages	6
DOIs	https://doi.org/10.1109/ICInfA.2013.6720491
Publication status	Published - 1 Dec 2013
Externally published	Yes
Event	2013 IEEE International Conference on Information and Automation, ICIA 2013 - Yinchuan, China Duration: 26 Aug 2013 → 28 Aug 2013

Conference

Conference	2013 IEEE International Conference on Information and Automation, ICIA 2013
Country/Territory	China
City	Yinchuan
Period	26/08/13 → 28/08/13

Keywords

control
dynamic modeling
onboard system
Quadrotor
UAV

ASJC Scopus subject areas

Information Systems

More information

10.1109/ICInfA.2013.6720491

Cite this

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AB - The UAV quadrotor is considerably difficult to be controlled due to its inherently unstable and complex multi-variable properties. To realize the control, a nonlinear dynamic model is firstly derived and formulated. A control approach employing hierarchical multiple-layer structure is then developed. The detailed hardware components, software as well as the working principle of the system are described. The entire UAV control system is tested and verified in actual flight tests.

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KW - dynamic modeling

KW - onboard system

KW - Quadrotor

KW - UAV

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M3 - Conference article published in proceeding or book

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BT - 2013 IEEE International Conference on Information and Automation, ICIA 2013

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Y2 - 26 August 2013 through 28 August 2013

ER -

Realization of the flight control for an indoor UAV quadrotor

Abstract

Conference

Keywords

ASJC Scopus subject areas

More information

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