Choice of the parameters of stabilization loop of the elastic maneuver unmanned aircraft

Аuthors

Parafes S. G.

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

e-mail: s.parafes@mail.ru

Abstract

The problem of formation of the stabilization loop of the maneuver unmanned aircraft for classes "air - to - surface” and "air - to - air" with the account of requirements of the aeroelastic stability with the automatic control system (ACS) is considered; the models and methods that are designed to solve this problem are given; the example of solving the problem, as well as the recommendations to provide the aeroelastic stability of the maneuver unmanned aircraft with ACS are considered.

Keywords:

unmanned aircraft, construction, automatic control system, stabilization loop, aeroelastic stability

Download