Dynamic behavior of the aircraft with effect of automatic control system elements.

Aviation technics and technology


Turkin I. K.1*, Kondrashev G. V.2**

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. State Machine Building Design Bureau «Vympel» by name I.I. Toropov, 90, Volokolamskoe shosse, Moscow, 125424, Russia

*e-mail: kafedra_602@mail.ru
**e-mail: termik5@mail.ru


We consider the elastic small-sized aircraft, rotating around its axis with a velocity of 3-5 M, is taken into account the intensive longitudinal loading and, consequently, the longitudinal acceleration of the aircraft. This takes into account the effect on the dynamic behavior of a model aircraft electromechanical rudder drive. A mathematical model simulating the operation of the major elements of the steering gear was developed. Dynamic equations of the spatial motion of an elastic aircraft modified in view of the developed mathematical model of rudder drive.


mathematical modelling; fluctuations; a steering drive; flight control


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