Solution to the problem of optimization control spatial movement of a light aircraft on the basis of the minimum principle of Pontryagin

Аuthors

Baranov V. N.^*, Zaw L. O.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: vnb36@mail.ru
**e-mail: zaw.lin@mail.ru

Abstract

The problem of developing and implementing the control algorithm of light aircraft, which must fend off the occasional atmospheric disturbance, causing a deviation from the trajectory of the flight task. Numerical solution of two-point boundary value problem of the canonical system of the Pontryagin maximum principle

Keywords:

equations of motion of center of mass of the aircraft, the terminal optimizing functional Hamiltonian, the conjugate variable.

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