Modeling of powered parafoil based on Kirchhoff motion equation

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.

[1]  David W. Carter,et al.  Autonomous Large Parafoil Guidance, Navigation, and Control System Design Status , 2007 .

[2]  Hua Liu,et al.  An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts , 2012 .

[3]  Nathan Slegers,et al.  Optimal Control for Terminal Guidance of Autonomous Parafoils , 2009 .

[4]  Nathan Slegers,et al.  Effects of Canopy-Payload Relative Motion on Control of Autonomous Parafoils , 2009 .

[5]  Yannick Aoustin,et al.  Control Algorithms of the Longitude Motion of the Powered Paraglider , 2012 .

[6]  Glen Brown,et al.  Apparent mass effects on parafoil dynamics , 1993 .

[7]  Yang Hua,et al.  Study on Powered-Parafoil Longitudinal Flight Performance with a Fast Estimation Model , 2013 .

[8]  Yoshimasa Ochi,et al.  Modeling and Simulation of Nonlinear Dynamics of a Powered Paraglider , 2008 .

[9]  T. Goodrick Simulation studies of the flight dynamics of gliding parachute systems , 1979 .

[10]  Nie Hong,et al.  Stochastic optimal control of flexible aircraft taxiing at constant or variable velocity , 2010 .

[11]  Gottfried Sachs,et al.  A High-fidelity Nonlinear Multibody Simulation Model for Parafoil Systems , 2003 .

[12]  Haitao Gao,et al.  Multi-objective global optimal parafoil homing trajectory optimization via Gauss pseudospectral method , 2013 .

[13]  T. Goodrick Comparison of simulation and experimental data for a gliding parachute in dynamic flight , 1981 .

[14]  David Carter,et al.  Autonomous Guidance, Navigation, and Control of Large Parafoils , 2005 .

[15]  T. Barrows Apparent Mass of Parafoils with Spanwise Camber , 2001 .