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Editor-in-Chief
Nikiforov
Vladimir O.
D.Sc., Prof.
Partners
FEATURES OF THE AIRCRAFT MOVEMENT IN A VERTICAL PLANE WITH THE LIMITED DRAFT OF THE ENGINE
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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
