Control Algorithm of the Angular Position of a Quadcopter Based on Statistical Analysis of Experimental Data

被引:1
|
作者
Veselov G.M. [1 ]
Voiskovskii A.P. [1 ]
Yakimenko V.A. [1 ]
机构
[1] Moscow Aviation Institute, Moscow
关键词
angular position control; copter; drone; orientation control; quadcopter;
D O I
10.3103/S1068798X21080256
中图分类号
学科分类号
摘要
Abstract: An algorithm is proposed for controlling the angular position of a quadcopter and establishing optimal (in terms of minimum time) orientation control in the absence of mathematical models of the copter and the perturbing factors that it experiences. The proposed approach to creating the control algorithm is based on Pontryagin’s maximum principle, the probability-guaranteed method, and experimental data. The results of employing the proposed approach on a test bench are outlined. © 2021, Allerton Press, Inc.
引用
收藏
页码:748 / 751
页数:3
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