Title :
Notice of Retraction
Design on Follow-Up Control System in Aerofoil Fatigue Experiment
Author :
Zhiyong Qu ; Zhengmao Ye
Author_Institution :
Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
Abstract :
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Certain three freedom motion system for afterbody motor fatigue experiment is presented. Inverse kinematics method is introduced to deduce the kinematics, where involve the stroke of cylinder and the afterbody distortion. Dynamics is then done to calculate the force of cylinder for giving the correct element choice based on Newton-Euler method. These things can help designer to find effective structure and applied stylebook in the later studies.
Keywords :
Newton method; aerospace components; aircraft control; fatigue; kinematics; motion control; Newton-Euler method; aerofoil fatigue experiment; afterbody distortion; afterbody motor fatigue experiment; cylinder stroke; follow-up control system design; inverse kinematics method; stylebook; three freedom motion system; Aerodynamics; Fatigue; Gravity; Joints; Kinematics;
Conference_Titel :
Circuits, Communications and System (PACCS), 2011 Third Pacific-Asia Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4577-0855-8
DOI :
10.1109/PACCS.2011.5990199
