Additional definition of the astatic control principle for sistems with coordinate-combine flight apparatus control

Аuthors

Pychkov A. M.

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

Abstract

In conditions of coordinate-combine flight-apparatus control the role channel is very important. The problem consists in high-dynamic realization of sign-alternative control signals. In this paper two solution variants of this problem are considered and described.

Keywords:

astatic control, coordinate-combine control, flight-apparatus, adaptation, algorithm.