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Modeling and Simulation of the Soft-Wing UAV
Abstract
DOF as a rigid body and the powered vehicle has pitching and yawing motion relative to the parafoil canopy. The dynamic response of soft-wing UAV was analyzed through simulation. With the engine power taken as input to control rising, and declining, the flight height of the soft-wing UAV can be adjusted. This 8 DOF mathematical model was proved to be rational with the analysis of
the simulation results, and a simulation foundation for the design of autonomous flight control algorithms is provided.
References
. Goodrick, T.F, “Theoretical study of the longitudinal stability of high-performance gliding airdrop systems,” AIAA Paper 1975-1394, 5th AIAA ADS Conference, Albuquerque, NM, November 17-19, 1975.
. Goodrick, T.F, “Simulation studies of the flight dynamics of gliding parachute systems,” AIAA Paper 1979-0417, 1979
. Yang Hua, “Study on Powered-Parafoil Longitudinal Flight Performance with a Fast Estimation Model, ” Journal of Aircraft, Vol. 50, No. 5, September–October 2013
. Nathan J. Slegers, “Effects of canopy-payload relative motion on control of autonomous parafoils,”Journal of Guidance, Control, and Dynamics, Vol. 33, No. 1, January-February 2010.
. Y Ochi and M Watanabe, “Modelling and simulation of the dynamics of a powered paraglider, ”Journal of Aerospace Engineering, 2011 225: 373
. Michael Ward, Sean Culpepper, “Parafoil Control Using Payload Weight Shift, ”AIAA Atmospheric Flight Mechanics Conference,13 - 16 August 2012, Minneapolis, Minnesota
. Chrystine M, “Modeling of Parafoil-Payload Relative Yawing Motion on Autonomous Parafoils, ” AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar,23 - 26 May 2011, Dublin, Ireland
. Oleg A. Yakimenko, “On the Development of a Sc alable 8-DoF Model for a Generic Parafoil-Payload Delivery System,” 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, 2005-1665.
. Slegers, N.and Costello, M, “Aspects of Control for Parafoil and Payload System,” Journal of Guidance, Control, and Dynamics, Volume 26,Number 6, pp.898-905, November-December 2003
. Mooij, E., Wijnands, Q. G. J. and Schat, B, “9 DoF Parafoil/Payload Simulator Development and Validation,” AIAA Modeling and Simulation Technologies Conference, Austin, Texas, August 2003.
. Michael Ward and Sean Culpepper, “Parametric Study of Powered Parafoil Flight Dynamics,” AIAA Atmospheric Flight Mechanics Conference, 13 - 16 August 2012, Minneapolis, Minnesota
. Michael Ward, Evaluation of Multi-body Parafoil Dynamics Using Distributed Miniature Wireless Sensors, AIAA Atmospheric Flight Mechanics Conference,08 - 11 August 2011, Portland, Oregon
. Om Prakash, “Trim and Stability Analysis of Parafoil/Payload System using Bifurcation Methods, ”18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, 2005-1666
. Ruan Xiaogang, “Dynamics Modeling and Analysis of a Reconfigurable Rotorcraft Unmanned Aerial Vehicle,” ROBOT, Vol.35, No.2, Mar., 2013.
. Brown, G. J., “Parafoil Steady Turn Resp onse to Control Input,” 12th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, London, UK, May 10-13 1993, pp. 248-254
. P. Lissaman and G. Brown,“Apparent mass effects on parafoil dynamics,”AIAA Paper 93-1236, May 1993.
. Cl.Toussaint and Ch. Cumer, “Flight dynamic modeling of the PBO parafoil using sparse preliminary flight test data” AIAA Aerodynamic Decelerator Systems (ADS) Conference 25-28 March 2013, Daytona Beach, Florida
. Prakash, O. and Ananthkrishnan, N., “Modeling and Simulation of 9-DOF Parafoil-Payload System Flight Dynamics,”AIAA Atmospheric Flight Mechanics Conference and Exhibit, Keystone, Colorado, 21-24 August 2006
DOI: http://dx.doi.org/10.21535%2FProICIUS.2014.v10.251
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