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
ITMO University, Saint Petersburg, 197101, Russian Federation; Scientific Design Bureau “Electroavtomatica”, Saint Petersburg, 198095, Russian Federation; Head of Chair; Head of Learning Scientific Center
V. N. Nikolaev
Southwest State University, Department of Information Systems and Technologies, Kursk; Professor
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.