Modeling of powered parafoil based on Kirchhoff motion equation

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• 作者：Erlin Zhu (1)
  Qinglin Sun (1)
  Panlong Tan (1)
  Zengqiang Chen (1)
  Xiaofeng Kang (2)
  Yingping He (3)
  
  1. College of Computer and Control Engineering ; Nankai University ; Tianjin ; 300071 ; China
  2. Military Representative Office of Aerospace Life-Support Industries Ltd. ; Xiangyang ; 441003 ; China
  3. AVIC Aerospace Life-Support Industries Ltd. ; Xiangyang ; 441003 ; China
  
• 关键词：Powered parafoil ; Relative motion ; Dynamic model ; Kirchhoff motion equation
• 刊名：Nonlinear Dynamics
• 出版年：2015
• 出版时间：January 2015
• 年：2015
• 卷：79
• 期：1
• 页码：617-629
• 全文大小：639 KB
• 参考文献：1. Zhang, M., Nie, H., Zhu, R.: Stochastic optimal control of flexible aircraft taxiing at constant or variable velocity. Nonlinear Dyn. 62(1鈥?), 485鈥?97 (2010)
  2. Liu, H., Guo, L., Zhang, Y.: An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts. Nonlinear Dyn. 67(3), 2081鈥?088 (2012) CrossRef
  3. Zhang, L., Gao, H., Chen, Z., Sun, Q.: Multi-objective global optimal parafoil homing trajectory optimization via Gauss pseudospectral method. Nonlinear Dyn. 72(1鈥?), 1鈥? (2013) CrossRef
  4. Carter, D., George, S., Hattis, P., et al.: Autonomous guidance, navigation and control of large parafoils. AIAA 1643, 1鈥?6 (2005)
  5. Carter, D., George, S., Hattis, P., et al.: Autonomous large parafoil guidance, navigation, and control system design status. AIAA 2514, 1鈥?5 (2007)
  6. Goodrick, T.: Comparison of simulation and experimental data for a gliding parachute in dynamic flight. AIAA 1924, 1鈥?2 (1981)
  7. Barrows, T.: Apparent mass of parafoil with spanwise camber. J. Aircr. 39(3), 445鈥?51 (2002) CrossRef
  8. Slegers, N., Yakimenko, O.: Optimal control for terminal guidance of autonomous parafoils. AIAA 2958, 1鈥?1 (2009)
  9. Muller, S., Wagner, O., Sachs, G.: A high-fidelity nonlinear multibody simulation model for parafoil systems. AIAA 2120, 1鈥?0 (2003)
  10. Xiong, J.: Research on the Dynamics and Homing Project of Parafoil System. National University of Defense Technology (in Chinese) (2005)
  11. Slegers, N.: Effects of canopy-payload relative motion on control of autonomous parafoils. J. Guid. Control Dyn. 33(1), 116鈥?25 (2010) CrossRef
  12. Aoustin, Y., Martinenko, Y.: Control algorithms of the longitude motion of the powered paraglider. In: Proceedings of the Biennial Conference on Engineering Systems Design and Analysis, pp. 775鈥?84 (2012)
  13. Yang, H., Song, L., Liu, C., et al.: Study on powered-parafoil longitudinal flight performance with a fast estimation model. J. Aircr. 50(5), 1660鈥?667 (2013) CrossRef
  14. Watanabe, M., Ochi, Y.: Modeling and simulation of nonlinear dynamics of a powered paraglider. AIAA 7418, 1鈥?6 (2008)
  15. Lissaman, P., Brown, G.: Apparent mass effects on parafoil dynamics. AIAA 1236, 233鈥?40 (1993)
  16. Goodrick, T.: Simulation studies of the flight dynamics of gliding parachute systems. AIAA 0417, 11鈥?6 (1979)
  
• 刊物类别：Engineering
• 刊物主题：Vibration, Dynamical Systems and Control
  Mechanics
  Mechanical Engineering
  Automotive and Aerospace Engineering and Traffic
  
• 出版者：Springer Netherlands
• ISSN：1573-269X

文摘

Powered parafoil is a kind of flexible wing vehicle, which is composed of traditional parafoil system and power plant. Considering the relative motion of canopy and payload, two coordinates are built separately to analyze the motion properties of canopy and payload. According to the Kirchhoff motion equation, eight degrees of freedom (DOF) dynamic model of powered parafoil is built, including six DOF motion of canopy and relative yaw and relative pitch motion of payload. The simulation focuses on the basic motions of gliding, turning, flare landing and the responses to the wind and power. The simulation results verify the validity of dynamic model of powered parafoil.