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- W2435711961 abstract "w u = cos CY,/(COS CY,~, + sin a,w,) 5,Y,z coordinates in FB X, Y, Z aerodynamic force components In this paper a general formulation for the analysis of XI, X2 state vectors hang-gliders dynamics and control is presented. The hangglider is modeled as a compound system made of wing and Greek symbols pilot. Static stability criteria are reviewed for a typical, indicative configuration. The small-perturbation dynamic CY angle of attack stability is investigated in the fixed and free-control cases /3 sideslip angle in analogy with the conventional aircraft. The frequency 7 glide angle response of the glider is evaluated and discussed. Unsteady 6, a longitudinal and lateral control angles aerodynamics effects are shown to play a role in stabilizing E twist angle the system." @default.
- W2435711961 created "2016-06-24" @default.
- W2435711961 creator A5068304446 @default.
- W2435711961 date "1989-08-14" @default.
- W2435711961 modified "2023-09-27" @default.
- W2435711961 title "Dynamics and control of hang-gliders" @default.
- W2435711961 cites W2048570505 @default.
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- W2435711961 doi "https://doi.org/10.2514/6.1989-3365" @default.
- W2435711961 hasPublicationYear "1989" @default.
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