Keyword: «turn – in»

TRIM BALANCE, STIFFNESS, CONTROLLABILITY, MANEVER CAPABILITY AND AUTOROTATION OF A HELICOPTER – TYPE UNMANNED AERIALVEHICLE

Authors:

Urii Onyshkin,

Vyacheslav Djaksbaev,

Edyard Marcinkevich

In this article the of results of trim calculations are examined, the assessment of a helicopter – type unmanned aerial vehicle stiffness and controllability is realized, autorotation capability is evaluated, examples of maneuvers calculating are given.

Keywords: unmanned aerial vehicle, helicopter, drive system, power plant, controllability, turn – in, pull up, nose dive