[1] Kowaleczko, G., “Apparent masses and inertia moments of the parafoil,” Journal of Theoretical and Applied Mechanics, 52, 2014.
[2] Devalla, V. and Prakash, O., “Developments in unmanned powered parachute aerial vehicle: a review,”IEEE Aerosp Electron Syst Mag 2014;29(11):6–20.
[3] Sun H, Sun Q and Luo S, “In-flight compound homing methodology of parafoil delivery systems under multiple constraints,” Aerosp Sci Technol 2018;79:85–104.
[4] Heise, M. and Muller, S., “Dynamic Modeling and Visualization of Multi-Body Flexible Systems,” AIAA Modeling and Simulation Technologies Conference and Exhibit, Providence, Rhode Island, August 2004.
[5] Slegers, N. and Costello, M., “Aspects Of Control For a Parafoil and Payload System,” Journal of Guidance, Control and Dynamics, 2003.
[6] Prakash, O. and Ananthkrishnan, N., “Modeling and Simulation of 9-DOF Parafoil-Payload System Flight Dynamics,” AIAA 2006-6130.
[7] Ward, M. and et al, “Parafoil Control Using Payload Weight Shift,”AIAA 2012-4738.
[8] ر. حاجیبابایی و ف. ثقفی،«استفاده از زاویه نصب عرضی بالچتری در هدایت و کنترل سامانه پارافویل-محموله،» چهاردهمین کنفرانس بینالمللی انجمن هوافضای ایران، تهران، 1393.
[9] Zipfel, P.H., Modeling and Simulation of Aerospace Vehicle Dynamics, Second Edition, University of Florida, 2007.
[10] Lingard, J.S., “Ram-Air Parachute Design,” 13th AIAA Aerodynamic Decelerator Systems Technology Conference, May 1995.
[11] Slotine, J.E. and Li, W., Applied Nonlinear Control, Prentice Hall, 1991.
)