Open AccessSimulation of quadcopter flight altitude stabilization system
Author(s) -
Mikhail Yu. Babich,
Mikhail M. Butaev,
Dmitry V. Pashchenko,
A.I Martyshkin,
Dmitry A. Trokoz
Publication year - 2020
Publication title -
nexo
Language(s) - English
Resource type - Journals
eISSN - 1995-9516
pISSN - 1818-6742
DOI - 10.5377/nexo.v33i02.10799
Subject(s) - quadcopter , rotation (mathematics) , position (finance) , control theory (sociology) , computer science , trajectory , aerospace engineering , simple (philosophy) , control engineering , simulation , control (management) , engineering , artificial intelligence , physics , finance , economics , philosophy , epistemology , astronomy
Recently, unmanned aerial vehicles have been an important part of scientific research in various fields. Quadrocopter is an unmanned aerial vehicle with four rotors, two of which rotate clockwise, the other two counterclockwise. Changing the speed of screw rotation allows you to control the movement of the apparatus. The article proposed and tested a mathematical model of a quadcopter. They presented the development of a simple control algorithm that allows to stabilize the height and angular position. The research results show the efficiency of the algorithm and the possibility of its practical implementation. The developed mathematical model can be used instead of a real quadcopter, which will significantly reduce the time during research, as well as avoid the quadrocopter damage, reducing the number of launches.