Criterions and computation method of distributed control signals limitations for flight-apparatus rule drives

Аuthors

Pychkov A. M.

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

Abstract

For unmanned flight apparatus executive machinery and ruling drives are the same for any contour of angle control. In this paper the problem of qualitative and correct control signals for ruling drives distribution is considered and solved.

Keywords:

invariability, adaptation, ruling drives, compensation, saturation, cinematic distribution, flight-apparatus