Autonomous control and trajectory tracking of quadrotor helicopter

The research on autonomous miniature flying robots is intensified considerable owing to the increasing interest of unmanned aerial vehicle (UAV). This paper summarizes the nonlinear dynamics of a quadrotor helicopter and the measurements of the aerodynamic parameters of its propeller. We propose an...

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Published in2012 IEEE International Conference on Computer Science and Automation Engineering Vol. 3; pp. 251 - 255
Main Authors Tianmiao Wang, Liewu Wang, Jianhong Liang, Yang Chen
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.05.2012
Subjects
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ISBN1467300888
9781467300889
DOI10.1109/CSAE.2012.6272949

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Abstract The research on autonomous miniature flying robots is intensified considerable owing to the increasing interest of unmanned aerial vehicle (UAV). This paper summarizes the nonlinear dynamics of a quadrotor helicopter and the measurements of the aerodynamic parameters of its propeller. We propose an attitude controller with the introduction of acceleration in error feedback, which will improve the stability and fast-tracking capability. In addition, a trajectory tracking controller is developed based on the along-track error and cross-track error feedback to track the waypoint. Finally, outdoor flight test results of attitude control and simple trajectory tracking are presented to verify the availability.
AbstractList The research on autonomous miniature flying robots is intensified considerable owing to the increasing interest of unmanned aerial vehicle (UAV). This paper summarizes the nonlinear dynamics of a quadrotor helicopter and the measurements of the aerodynamic parameters of its propeller. We propose an attitude controller with the introduction of acceleration in error feedback, which will improve the stability and fast-tracking capability. In addition, a trajectory tracking controller is developed based on the along-track error and cross-track error feedback to track the waypoint. Finally, outdoor flight test results of attitude control and simple trajectory tracking are presented to verify the availability.
Author Liewu Wang
Tianmiao Wang
Yang Chen
Jianhong Liang
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  surname: Yang Chen
  fullname: Yang Chen
  organization: Dept. of Mech. Eng. & Autom., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
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Snippet The research on autonomous miniature flying robots is intensified considerable owing to the increasing interest of unmanned aerial vehicle (UAV). This paper...
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StartPage 251
SubjectTerms Acceleration
aerodynamic parameter
Aerodynamics
Angular velocity
Attitude control
dynamics
Helicopters
Propellers
quadrotor helicopter
Trajectory
trajectory tracking
Title Autonomous control and trajectory tracking of quadrotor helicopter
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