Identyfikatory
Warianty tytułu
Języki publikacji
Abstrakty
This paper presents a useful method of determination of additional forces and moments which have to be taken into account in analysis of a parafoil or paraglider flight dynamics. They are produced by apparent masses and apparent inertia moments of the air. These masses and inertia moments have strong effects on the flight dynamics of a lightly-loaded parafoil. The equations of motion for the parafoil-payload system are also shortly presented. An analytical method of calculating of the apparent masses and inertia moments is shown. Exemplary results are presented.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
605--616
Opis fizyczny
Bibliogr. 7 poz., rys., tab.
Twórcy
Bibliografia
- 1. Barrows T., 2002, Apparent mass of parafoils with spanwise camber, Journal of Aircraft, 39, 3, 445-451
- 2. Dobrokhodov V., Yakimenko O., Junge Ch., 2003, Six-degree-of-freedom model of a controlled circular parachute, Journal of Aircraft, 40, 3, 482-493
- 3. Gamble J., 1998, A mathematical model for calculating the flight dynamics of a general parachute-payload system, NASA Technical Note, NASA TN D-4859
- 4. Lissaman P., Brown G., 1993, Apparent mass effects on parafoil dynamics, AIAA Paper, AIAA--93-1236
- 5. Ochi Y., Watanabe M., 2011, Modeling and simulation of the dynamics of a powered paraglider, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 225, 4, 373-386
- 6. Toglia Ch., Vendittelli M., 2010, Modeling and motion analysis of autonomous paragliders, Technical Report, Universita di Roma
- 7. Tweddle B., 2006, Simulation and control of guided ram air parafoils, Technical Report, University of Waterloo
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-7c0ece82-bdc4-48e6-a9c7-5369da8b7c1e