Journal of Theoretical
and Applied Mechanics
25, 1-2, pp. 265-271, Warsaw 1987
and Applied Mechanics
25, 1-2, pp. 265-271, Warsaw 1987
Symulacja sterowanego ruchu samolotu podczas startu i lądowania
The model of airplane flight control system during the take-off and landing has been presented in this paper. The derivation of formulae describing the dynamics of airplanes flight during the take-off and landing has been proposed. The results of simulating these phases of flight by the digital computer has been shown.