DocumentCode
2839904
Title
Notice of Retraction
Dynamics analysis and simulation of 9 DOF unmanned powered parachute based on Kane method
Author
Zhou Hong-xin ; Chen Zi-li ; Jiang Tao
Author_Institution
Ordnance Eng. Coll., Shijiazhuang, China
Volume
6
fYear
2010
fDate
22-24 Oct. 2010
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.
A formulation based on Kane Equation and kinematics of unmanned powered parachute was educed, which includes free and constraintmode. The velocities of unmanned powered parachute´s parafoil and vehicalvehicle which linked to base joint were chosen as generalized velocities. The partial velociy and the partial angular velocity of parafoil and vehical were educed. Develop a 9DOF dynamics model of a unmanned powered parachute. The numerical simulation of the dynamics was carried out by using MATLAB software.The simulation results show that the unmanned powered parachute has passive and constraint characteristics.The dynamics can provide theoretical bases for analysis and simulation of the umanned powered prachute control and so forth.
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.
A formulation based on Kane Equation and kinematics of unmanned powered parachute was educed, which includes free and constraintmode. The velocities of unmanned powered parachute´s parafoil and vehicalvehicle which linked to base joint were chosen as generalized velocities. The partial velociy and the partial angular velocity of parafoil and vehical were educed. Develop a 9DOF dynamics model of a unmanned powered parachute. The numerical simulation of the dynamics was carried out by using MATLAB software.The simulation results show that the unmanned powered parachute has passive and constraint characteristics.The dynamics can provide theoretical bases for analysis and simulation of the umanned powered prachute control and so forth.
Keywords
aerodynamics; mathematics computing; remotely operated vehicles; robot kinematics; space vehicles; vehicle dynamics; 9 DOF unmanned powered parachute; 9DOF dynamic model; Kane equation; MATLAB software; numerical simulation; parachute parafoil; partial angular velocity; vehical vehicle; Silicon; Dnamics modeling; Kane method; MATLAB simulation; Unmanned Powered Parachute;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location
Taiyuan
Print_ISBN
978-1-4244-7235-2
Type
conf
DOI
10.1109/ICCASM.2010.5620761
Filename
5620761
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