title: Ð¡ÑÐ°Ð²Ð½Ð¸ÑÐµÐ»ÑÐ½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· Ð°Ð»Ð³Ð¾ÑÐ¸ÑÐ¼Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸ÐµÐ¹ ÐÐÐÐ Ð² Ð½ÐµÐ¾Ð¿ÑÐµÐ´ÐµÐ»ÐµÐ½Ð½ÑÑ ÑÑÐµÐ´Ð°Ñ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð½ÐµÑÑÑÐºÐ¾Ð¹ Ð»Ð¾Ð³Ð¸ÐºÐ¸ Ð¸ ÐºÐ²Ð°Ð·Ð¸Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½ÑÑ Ð·Ð°ÐºÐ¾Ð½Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ
title: Comparative analysis of UAV orientation control algorithms based on fuzzy logic and quasi-optimal control laws
Creators: name: ÐÐ¾ÑÑÐ¾Ð³Ð»Ð¾ÑÐ¾Ð², ÐÐ½Ð´ÑÐµÐ¹
name: ÐÐ°Ð·Ð°ÑÐµÐ½ÐºÐ¾, Ð¡ÐµÑÐ³ÐµÐ¹
name: ÐÐµÑÑÐµÑ, ÐÐ»Ð°Ð´Ð¸Ð¼Ð¸Ñ
name: "Ð¡Ð¸ÑÑÐµÐ¼Ð½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· Ð² Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ð¸ Ð¸ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ð¸", Ð¼ÐµÐ¶Ð´ÑÐ½Ð°ÑÐ¾Ð´Ð½Ð°Ñ Ð½Ð°ÑÑÐ½Ð¾-Ð¿ÑÐ°ÐºÑÐ¸ÑÐµÑÐºÐ°Ñ ÐºÐ¾Ð½ÑÐµÑÐµÐ½ÑÐ¸Ñ (27; 2023; Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³)
Publisher: name: ÐÐÐÐÐ¢ÐÐ¥-ÐÐ ÐÐ¡Ð¡
Year: 2024
Subjects: ÐÐµÑÐ°ÑÐµÐ»ÑÐ½ÑÐµ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑ Ð±ÐµÑÐ¿Ð¸Ð»Ð¾ÑÐ½ÑÐµ
ÐÐ°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ
Ð´Ð¸Ð½Ð°Ð¼Ð¸ÑÐµÑÐºÐ¸Ðµ ÑÐ¸ÑÑÐµÐ¼Ñ
ÑÐ¸Ð½ÑÐµÐ· ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ
Ð½ÐµÑÑÑÐºÐ¸Ð¹ Ð»Ð¾Ð³Ð¸ÑÐµÑÐºÐ¸Ð¹ Ð²ÑÐ²Ð¾Ð´
Ð¸Ð½ÑÐµÐ»Ð»ÐµÐºÑÑÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ñ
unmanned aerial vehicles
dynamic systems
control synthesis
fuzzy inference
intellectualization

description: ÐÑÐ»ÑÑÐ¸ÑÐ¾ÑÐ¾ÑÐ½ÑÐµ Ð±ÐµÑÐ¿Ð¸Ð»Ð¾ÑÐ½ÑÐµ Ð»ÐµÑÐ°ÑÐµÐ»ÑÐ½ÑÐµ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑ ÑÑÐ½ÐºÑÐ¸Ð¾Ð½Ð¸ÑÑÑÑ Ð² ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐµÐ¶Ð¸Ð¼Ð°Ñ Ð¿Ð¾Ð»ÐµÑÐ°, ÑÑÐ¾ Ð¾Ð¿ÑÐµÐ´ÐµÐ»ÑÐµÑ Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼Ð¾ÑÑÑ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸Ñ Ð¼Ð½Ð¾Ð³Ð¾ÑÐµÐ¶Ð¸Ð¼Ð½Ð¾Ð³Ð¾ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ. Ð ÑÑÐ»Ð¾Ð²Ð¸ÑÑ Ð½ÐµÑÐ¿Ð¾ÐºÐ¾Ð¹Ð½Ð¾Ð¹ Ð°ÑÐ¼Ð¾ÑÑÐµÑÑ Ð¸Ñ ÑÐ¸ÑÑÐµÐ¼Ð° ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð´Ð¾Ð»Ð¶Ð½Ð° Ð¾Ð±ÐµÑÐ¿ÐµÑÐ¸Ð²Ð°ÑÑ Ð²ÑÑÐ¾ÐºÐ¾Ðµ ÐºÐ°ÑÐµÑÑÐ²Ð¾ ÑÑÐ°Ð±Ð¸Ð»Ð¸Ð·Ð°ÑÐ¸Ð¸, Ð½Ð¾ Ð¿ÑÐ¸ ÑÑÐ¾Ð¼ Ð±ÑÑÑ Ð´Ð¾ÑÑÐ°ÑÐ¾ÑÐ½Ð¾ Ð¿ÑÐ¾ÑÑÐ¾Ð¹ Ð´Ð»Ñ Ð²Ð¾Ð·Ð¼Ð¾Ð¶Ð½Ð¾ÑÑÐ¸ ÐµÐµ ÑÐµÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ð¸. Ð­ÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾Ðµ Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ð¸Ðµ ÑÐ¸ÑÑÐµÐ¼Ñ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð¼Ð¾Ð¶Ð½Ð¾ ÑÐµÐ°Ð»Ð¸Ð·Ð¾Ð²Ð°ÑÑ Ñ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¸ÐµÐ¼ Ð¼ÐµÑÐ¾Ð´Ð° ÐºÐ²Ð°Ð·Ð¸Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½Ð¾Ð³Ð¾ ÑÐ¸Ð½ÑÐµÐ·Ð° Ð·Ð°ÐºÐ¾Ð½Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ ÑÐµÐ´ÑÐºÑÐ¸Ð¸ Ð·Ð°Ð´Ð°ÑÐ¸ ÐÐ°Ð³ÑÐ°Ð½Ð¶Ð° Ðº Ð¸Ð·Ð¾Ð¿ÐµÑÐ¸Ð¼ÐµÑÑÐ¸ÑÐµÑÐºÐ¾Ð¹ Ð·Ð°Ð´Ð°ÑÐµ Ñ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ° Ð½ÐµÑÑÑÐºÐ¾Ð¹ Ð»Ð¾Ð³Ð¸ÐºÐ¸. Ð ÑÐ°Ð±Ð¾ÑÐµ Ð¿ÑÐ¾Ð²Ð¾Ð´Ð¸ÑÑÑ ÑÑÐ°Ð²Ð½Ð¸ÑÐµÐ»ÑÐ½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· Ð°Ð»Ð³Ð¾ÑÐ¸ÑÐ¼Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð¾ÑÐ¸ÐµÐ½ÑÐ°ÑÐ¸ÐµÐ¹ ÐÐÐÐ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ ÐºÐ²Ð°Ð·Ð¸Ð¾Ð¿ÑÐ¸Ð¼Ð°Ð»ÑÐ½ÑÑ Ð·Ð°ÐºÐ¾Ð½Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ñ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½Ð¸ÐµÐ¼ Ð½ÐµÑÑÑÐºÐ¾Ð¹ Ð»Ð¾Ð³Ð¸ÐºÐ¸ Ð¸ Ð¸Ð·Ð²ÐµÑÑÐ½Ð¾Ð³Ð¾ ÑÐµÑÐµÐ½Ð¸Ñ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð½ÐµÑÑÑÐºÐ¾Ð³Ð¾ PID-ÑÐµÐ³ÑÐ»ÑÑÐ¾ÑÐ°.
description: Multi-rotor unmanned aerial vehicles operate in various flight modes, which determines the need to use multi-mode control. In a turbulent atmosphere, their control system should provide high-quality stabilization, but at the same time be simple enough to be able to implement it. The effective construction of a control system can be implemented using the method of quasi-optimal synthesis of control laws based on the reduction of the Lagrange problem to an isoperimetric problem and the condition of the maximum of the generalized power function, as well as using the fuzzy logic apparatus. The paper presents a comparative analysis of UAV orientation control algorithms based on quasi-optimal control laws using fuzzy logic and a known solution based on a fuzzy PID controller.