Optimal control of light airplane during flight tests

Аuthors

Baranov V. N.^*, Li B. K.^**

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

*e-mail: vnb36@mail.ru
**e-mail: buiqangly@mail.ru

Abstract

A problem of non-iteration synthesis is solved in the paper to generate a control algorithm for a light airplane to go through flight tests. It is proved that the algorithm suggested in the paper is practically the same as optimal control algorithm basing on Pontryagins maximum principle.

Keywords:

light airplane; crash monitoring; optimization of control