Keyword: «drive system»
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
The article deals with the examples of the most frequently used computer software for tackling five problems in navigational calculations for helicopter flight.