Detail publikačního výsledku

Modelling and Control of a Quadrocopter

ŠOLC, F.

Originální název

Modelling and Control of a Quadrocopter

Anglický název

Modelling and Control of a Quadrocopter

Druh

Článek recenzovaný mimo WoS a Scopus

Originální abstrakt

The paper describes model and development of full control of a qudrotor aerial robot. The mathematical model of quadrotor is nonlinear system based on Newton law of motion of rigid body. Control system of the quadrotor is designed with help of state variable approach and also with help of corresponding physical approach which was inspired by the former one. Quality of model and its control is tested by simulation and on a real flying model as well.

Anglický abstrakt

The paper describes model and development of full control of a qudrotor aerial robot. The mathematical model of quadrotor is nonlinear system based on Newton law of motion of rigid body. Control system of the quadrotor is designed with help of state variable approach and also with help of corresponding physical approach which was inspired by the former one. Quality of model and its control is tested by simulation and on a real flying model as well.

Klíčová slova

quadrocopter, quadrotor, control, flying robot, VTOL aircraft, robot

Klíčová slova v angličtině

quadrocopter, quadrotor, control, flying robot, VTOL aircraft, robot

Autoři

ŠOLC, F.

Rok RIV

2011

Vydáno

30.12.2010

Nakladatel

University of Defence

Místo

Brno

ISSN

1802-2308

Periodikum

Advances in Military Technology

Svazek

5

Číslo

2

Stát

Česká republika

Strany od

29

Strany do

38

Strany počet

9

BibTex

@article{BUT49945,
  author="František {Šolc}",
  title="Modelling and Control of a Quadrocopter",
  journal="Advances in Military Technology",
  year="2010",
  volume="5",
  number="2",
  pages="29--38",
  issn="1802-2308"
}