Journal
Scientific and technical journal of information technologies, mechanics and optics
UDK681.5.01
Issue:3 (67)
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FEATURES OF THE AIRCRAFT MOVEMENT IN A VERTICAL PLANE WITH THE LIMITED DRAFT OF THE ENGINE
Annotation
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.
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