Abstract
The subject of this paper is to analyze, create a dynamic mathematical model and, on this basis, conduct simulation tests of the control system used in unmanned aerial vehicles. The key objective of the work is to develop a mathematical model of a control system based on the conducted studies of P, PI and PID regulators. The summary of this article are selected simulation tests of the proposed unmanned aerial vehicle (UAV) control system based on the analysis performed, the mathematical model developed for the dynamic control system and based on them, drawing practical conclusions.
Highlights
Stabilizing the ceiling of unmanned aerial vehicle UAV is a key issue on the way to ensuring the safety of its operation in an autonomous mode
The mathematical model used for the analysis of the proposed unmanned aerial vehicle control system was formulated for a flying platform, powered by four electric engines, which were located on the vertical axis
The mathematical model of the UAV control system has been simulated in the Matlab/Simulink environment
Summary
Stabilizing the ceiling of unmanned aerial vehicle UAV is a key issue on the way to ensuring the safety of its operation in an autonomous mode. An additional factor increasing the complexity of the issue is the fact that in most practical solutions, due primarily to low costs, the stabilization of the ceiling of the said class of aircraft is carried out with the aid of ultrasonic sensors. The mathematical model used for the analysis of the proposed unmanned aerial vehicle control system was formulated for a flying platform, powered by four electric engines, which were located on the vertical axis. In specialist nomenclature, this kind of platform is called the quadcopter. Brushless motors were used, performing 1600 revolutions per 1 [V] power, with engines of this type being used as the main platform drive [4], [5]
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