A Review of Control Algorithms for Quadrotor

The unmanned aerial vehicle (UAV) is subject to various disturbances during the flight, such as the noise and drift of the sensor, strong wind and turbulence, and model variation caused by the excessive inclination. These would seriously affect the flight quality of the aircraft, so UAV control tech...

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Bibliographic Details
Published in2018 IEEE International Conference on Information and Automation (ICIA) pp. 951 - 956
Main Authors Han, Bo, Zhou, Yimin, Deveerasetty, Kranthi Kumar, Hu, Chaofang
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.08.2018
Subjects
Aircraft
Attitude control
Control systems
Heuristic algorithms
Intelligent controller
Linear controller
Mathematical model
Nonlinear controller
Quadrotor
Uncertainty
Unmanned aerial vehicles
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Summary:The unmanned aerial vehicle (UAV) is subject to various disturbances during the flight, such as the noise and drift of the sensor, strong wind and turbulence, and model variation caused by the excessive inclination. These would seriously affect the flight quality of the aircraft, so UAV control technology is particularly important. The quadrotor UAV is an important platform for control technology research, which has become the ideal choice for the synthesis and analysis of the control algorithm due to its nonlinearity and under-actuated properity. This paper briefly reviews the dynamic modeling of the quad-rotor, and compares the linear control algorithm, nonlinear control algorithm and intelligent control algorithm. Then the challenges and development trends of the quadrotor UAV control algorithm are summarized.
DOI:10.1109/ICInfA.2018.8812437