Journal of Theoretical
and Applied Mechanics
25, 1-2, pp. 227-233, Warsaw 1987
and Applied Mechanics
25, 1-2, pp. 227-233, Warsaw 1987
Modelowanie samolotu jako zamkniętego systemu sterowania
The paper presents a method of investigation and a model of an airplane flight control system. It includes: derivation of formulae describing the system and their final form, discussion of the structure of the computer simulating program, and presentation of the results obtained with the program.