FEATURES OF THE AIRCRAFT MOVEMENT IN A VERTICAL PLANE WITH THE LIMITED DRAFT OF THE ENGINE

B. . Vidin, O. . Uljanova


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Abstract

 

The nonlinear system of differential equations describing movement of the weights center of the aircraft in a
vertical plane at a rectilinear trajectory is researched. Estimations on speed and range values depending on
restrictions on an engine draft control resource are received.

Keywords: aircraft dynamics, control resource, restrictions
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