To the problem of flight dynamics

Abstract

New variational method is applied to solve the following problem: optimize the trajectory of the longitudinal motion of the mass center of aircraft flying in vertical plain from the initial point of atmospheric space to a predetermined point on the Earth surface. The main content of this work is that the complicated nonlinear boundary value problem is obtained by a finite number of arithmetic operations. These results confirm the numerical simulation effective examination techniques. Refs 3. Tables 1.