Propeller Force-Constant Modeling for Multirotor UAVs from Experimental Estimation of Inflow Velocity

Design and simulation of an unmanned aerial vehicle (UAV) highly depends on the thrust produced by a motor-propeller combination. The aim of this paper is to model a generalized mathematical relationship between the motor RPM and the corresponding thrust generated for the preliminary design process...

Full description

Saved in:
Bibliographic Details
Main Authors: Gaurang Gupta, Shaaban Abdallah
Format: Article
Language:English
Published: Wiley 2018-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2018/9632942
Tags: Add Tag
No Tags, Be the first to tag this record!