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

Aviation technics and technology


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


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