Estimation of velocity characteristics of low-sized uav with electric engine

Аuthors

Zakhartchenko V. F.¹, Targamadze R. C.², Frolov E. A.²

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. UAV Centr Lavochkin Science and Production Association,

Abstract

There is given the estimation the velocity interval of UAV horizontal flight for the given duration and the weight parameters of the vehicle. There is considered the UAV with handoff type of take off. After the electric engine with propeller start the initial velocity is created providing the necessary climb rate. The landing is carried out with help of parachute.

Keywords:

unmanned aerial vehicle, velocity of flight, handoff type of take off, electric engine with propeller, climbing capacity, necessary power, accumulator capacity, flights time.