PECULIARITIES OF AIRCRAFT MOVEMENT IN VERTICAL PLANE IN NONEQUILIBRIUM REGIME WITH THE ACCOUNT FOR LIMITED CONTROL RESOURCES
Federal State Unitary Enterprise «Saint Petersburg Scientific Design Bureau “Electroavtomatica”» after P. A. Efimov; Deputy Chief constructor
I. O. Zharinov
Stock Company "Experimental Design Bureau "Electroavtomatika" named after P.A. Yefimov", Saint Petersburg, 198095, Russian Federation; ITMO University, Saint Petersburg, 197101, Russian Federation; Head of Learning Scientific Center; Head of Chair
V. N. Nikolaev
Southwest State University, Department of Information Systems and Technologies, Kursk; Professor
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Abstract. 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.
Keywords:
aircraft dynamics, control resources, restrictions.
