Journal of Theoretical
and Applied Mechanics

25, 1-2, pp. 257-264, Warsaw 1987

Model matematyczny wyznaczania funkcji sterowania samolotem w pętli

Wojciech Blajer, Jan Parczewski

An airplane programed motion in loop has been studied. The airplane center of gravity has been postulated to perform a vertical loop as an ideal circle. A mathematical model for finding such a function of horizontal tail controlling that the motion be compliant with the program constraint is presented. The airplane was modelled as a rigid body with rigid flying controls.