Modelling and simulation of the dynamics of a powered paraglider

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 225, Issue 4, 2011, Pages 373-386

  Ochi, Y ^a   Watanabe, M ^a  

^a NATIONAL DEFENSE ACADEMY   (Japan)

Author keywords

Flight control; Internal forces; Linear dynamics; Non linear dynamics; Paraglider; State transformation

Indexed keywords

FLIGHT CONTROL; INTERNAL FORCES; LINEAR DYNAMICS; NON-LINEAR DYNAMICS; PARAGLIDER; STATE TRANSFORMATION;

COMPUTER SIMULATION; DYNAMIC MODELS; DYNAMICS; EQUATIONS OF MOTION; EQUATIONS OF STATE; FLIGHT SIMULATORS; LINEAR TRANSFORMATIONS;

MATHEMATICAL TRANSFORMATIONS;

EID: 79956114985     PISSN: 09544100     EISSN: 20413025     Source Type: Journal    
DOI: 10.1177/09544100JAERO888     Document Type: Conference Paper

References (17)

1. Azuma, A. Flight dynamics of paraglider, Lecture Note, 1994 (University of Tokyo, Tokyo).
2. Li, Y. and Nahon, M. Modeling and simulation of airship dynamics. J. Guid. Control Dyn., 2007, 30(6), 1691-1700. (Pubitemid 350218795)
3. Slegers, N. andCostello,M.Model predictive control of a parafoil and payload system. J. Guid. Control Dyn., 2005, 28(4), 816-821. (Pubitemid 41049826)
4. Doherr, K. F. and Schilling, H. Nine-degree-of-freedom simulation of rotating parachute systems. J. Aircr., 1992, 29(5), 774-781. (Pubitemid 23558715)
5. Slegers, N. and Costello, M. Aspects of control for a parafoil and payload system. J. Guid. Control Dyn., 2003, 26(6), 898-905.
6. Mooij, E., Wijnands, Q. G. J., and Schat, B. 9 dof parafoil/payload simulator development and validation. In Proceedings of the AIAA Modeling and Simulation Technologies Conference, Austin, Texas, 11-14 August 2003, pp. 1-12, AIAA paper 2003-5459.
7. Yakimenko, O. A. On the development of a scalable 8-DOF model for a generic parafoil-payload delivery system. In Proceedings of the AIAA Aerodynamic Decelerator Systems Conference, Munich, Germany, 23-26 May 2005, pp. 642-654, AIAA paper 2005-1665. (Pubitemid 41810844)
8. Hur, G.-B. and Valasek, J. System identification of powered parafoil-vehicle from flight data. In Proceedings of the AIAA Atmospheric Flight Mechanics Conference, Austin, Texas, 11-14 August 2003, pp. 1-7, AIAA paper 2003-5539.
9. Muller, S.,Wagner,O., and Sachs, G. A high-fidelity nonlinear multibody simulation model for parafoil systems. In Proceedings of the AIAA Aerodynamic Decelerator Systems Conference, Monterey, California, 19-22 May 2003, pp. 149-158, AIAA paper 2003-2120.
10. Akasaka, T., Beppu, G., and Azuma, A. An investigation of paraglider's turn mechanism (in Japanese). J. Jpn. Soc. Aeronaut. Space Sci., 1999, 47(540), 9-15.
11. Slegers, N. Effects of canopy-payload relative motion on control of autonomous parafoils. J . Guid. Control Dyn., 2010, 33(1), 116-125.
12. Wise, K. Dynamics of a UAV with parafoil under powered flight. In Proceedings of the AIAA Guidance, Navigation, and Control Conference, Keystone, Colorado, 21-24 August 2006, pp. 1-23, AIAA paper 2006-6795.
13. Redelinghuys, C. A flight simulation algorithm for a parafoil suspending an air vehicle. J. Guid. Control Dyn., 2007, 30(3), 791-803. (Pubitemid 46848338)
14. Azuma, A. Characteristics of paraglider (in Japanese), 1996 (JASPA, Tokyo).
15. Watanabe, M. and Ochi, Y. Modeling and simulation of nonlinear dynamics of a powered paraglider. In Proceedings of the AIAA Guidance, Navigation, and Control Conference, Honolulu, Hawaii, 18-21 August 2008, pp. 1-16, AIAA paper 2008-7418.
16. Ochi, Y., Kondo, H., andWatanabe, M. Linear dynamics and PID flight control of a powered paraglider. In Proceedings of the AIAA Guidance, Navigation, and ControlConference, Chicago, Illinois, 10-13August 2009, pp. 1-13, AIAA paper 2009-6318.
17. Kothare, M.V.,Campo,P. J.,Morari, M., and Nett, C. N. A unified framework for the study of anti-windup design. Automatica, 1994, 30(12), 1869-1883. (Pubitemid 124008076)