Journal
Scientific and technical journal «Priborostroenie»
UDK681.5.01
Issue:10 (53)
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PECULIARITIES OF AIRCRAFT MOVEMENT IN VERTICAL PLANE IN NONEQUILIBRIUM REGIME WITH THE ACCOUNT FOR LIMITED CONTROL RESOURCES
Annotation
System of nonlinear differential equations for aircraft mass center movement in vertical plane is analyzed for the case of linear path. Estimates are derived for velocity and flight range depending on control restrictions.
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