A model of quadrotor UAV power consumption and its performance across a range of flight conditions

This thesis presents a parametric model of quadrotor power consumption and characterizes the performance of this model in hardware experiments. Like other existing power models that have been used both for quadrotors and general rotorcraft, it can be expressed as the sum of four terms---induced, parasitic, profile, and climb power---that depend on estimates of the aerodynamic forces and moments acting on the quadrotor. The model's accuracy was measured across a wide range of flight conditions. The results of an ablation study to show the relative contribution of each term are presented, concluding that the contribution strongly depends on the ground velocity of the quadrotor. Both the dataset and code are freely available as a benchmark to facilitate future work in this area.

Name thesis:degree_name

M.S.

Level thesis:degree_level

Thesis

Discipline thesis:degree_discipline

Aerospace Engineering

Grantor

University of Illinois at Urbana-Champaign

Year dc:date

2020

Author dc:creator

• Faustino, Alexander B.

Contributors dc:contributor

• Bretl, Timothy

• Quadrotor UAVs
• UAV power modeling

Statement dc:rights

• Copyright 2019 Alexander Faustino

Language dc:language

en

Handle dc:identifier

http://hdl.handle.net/2142/106288

OAI identifier oai:identifier

oai:www.ideals.illinois.edu:2142/106288