Journal of Theoretical
and Applied Mechanics
18, 4, pp. 577-586, Warsaw 1980
and Applied Mechanics
18, 4, pp. 577-586, Warsaw 1980
Nowa metoda syntezy układu sterowania flatterem profilu
In the paper the theory of modal control was applied to the syntesis of the regulator of aeroelastic vibrations in the classical model of wing. The linear unsteady aerodynamics was assumed. The linearity and stationarity of the system have been obtained by means of Jones' approximation of Wagner's function.