title: Ð£Ð¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ðµ Ð¿Ð¾Ð»ÑÑÐ¾Ð¼ Ð²ÐµÑÑÐ¾Ð»ÑÑÐ° Ð¿Ð¾ Ð·Ð°Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ð¸ Ð² Ð¿ÑÐ¾Ð´Ð¾Ð»ÑÐ½Ð¾Ð¹ Ð¸ Ð±Ð¾ÐºÐ¾Ð²Ð¾Ð¹ Ð¿Ð»Ð¾ÑÐºÐ¾ÑÑÐ¸
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð±Ð°ÐºÐ°Ð»Ð°Ð²ÑÐ°
titleType: Subtitle
title: Helicopter flight control along a given trajectory in the longitudinal and lateral planes
Creators: name: ÐÐ¾ÑÐºÐ²Ð¸Ð½, ÐÐ¸ÐºÐ¸ÑÐ°
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2021
Subjects: matlab
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structured data
data analysis
control synthesis
centralized controller
decentralized controller
transients

description: ÐÐ±ÑÐµÐºÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ: Ð¼Ð°ÑÐµÐ¼Ð°ÑÐ¸ÑÐµÑÐºÐ°Ñ Ð¼Ð¾Ð´ÐµÐ»Ñ Ð²ÐµÑÑÐ¾Ð»ÑÑÐ° ÑÐµÐ¼ÐµÐ¹ÑÑÐ²Ð° ÐÐ-1. ÐÑÐµÐ´Ð¼ÐµÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ: ÑÐ¸Ð½ÑÐµÐ· ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐ¸Ð¿Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð¿ÑÐ¾Ð´Ð¾Ð»ÑÐ½ÑÐ¼ Ð¸ Ð±Ð¾ÐºÐ¾Ð²ÑÐ¼ Ð´Ð²Ð¸Ð¶ÐµÐ½Ð¸ÐµÐ¼ Ð²ÐµÑÑÐ¾Ð»ÑÑÐ° Ð¿Ð¾ Ð·Ð°Ð´Ð°Ð½Ð½Ð¾Ð¹ ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ð¸. Ð¦ÐµÐ»Ñ Ð´Ð¸Ð¿Ð»Ð¾Ð¼Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ â Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°ÑÑ Ð¿Ð¾Ð²ÐµÐ´ÐµÐ½Ð¸Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ Ð²ÐµÑÑÐ¾Ð»ÑÑÐ° Ð¿ÑÐ¸ Ð´Ð²Ð¸Ð¶ÐµÐ½Ð¸Ð¸ Ð² Ð¿ÑÐ¾Ð´Ð¾Ð»ÑÐ½Ð¾Ð¹ Ð¸ Ð±Ð¾ÐºÐ¾Ð²Ð¾Ð¹ Ð¿Ð»Ð¾ÑÐºÐ¾ÑÑÑÑ Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ Ð¸Ð½ÑÑÑÑÐ¼ÐµÐ½ÑÐ°Ð»ÑÐ½ÑÑ ÑÑÐµÐ´ÑÑÐ² Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ñ MATLAB. ÐÑÐ¸ Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ð¸Ð¸ ÑÐ°Ð±Ð¾ÑÑ Ð½ÐµÐ¾Ð±ÑÐ¾Ð´Ð¸Ð¼Ð¾ Ð²ÑÐ¿Ð¾Ð»Ð½Ð¸ÑÑ: â¢ ÑÐ¸Ð½ÑÐµÐ· ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐ¸Ð¿Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ; â¢ Ð²Ð¸Ð·ÑÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ñ Ð´Ð°Ð½Ð½ÑÑ; â¢ Ð°Ð½Ð°Ð»Ð¸Ð· Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÑ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐ¾Ð². Ð ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÐµ Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ð¸Ñ Ð²ÑÐ¿ÑÑÐºÐ½Ð¾Ð¹ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð¹ ÑÐ°Ð±Ð¾ÑÑ Ð±ÑÐ»Ð° ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÐ½Ð° Ð¼Ð¾Ð´ÐµÐ»Ñ Ð²ÐµÑÑÐ¾Ð»ÑÑÐ° Ñ Ð¸ÑÑÐ¾Ð´Ð½ÑÐ¼ Ð½Ð°Ð±Ð¾ÑÐ¾Ð¼ Ð´Ð°Ð½Ð½ÑÑ. ÐÑÐ»Ð¸ ÑÐ¸Ð½ÑÐµÐ·Ð¸ÑÐ¾Ð²Ð°Ð½Ñ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÐµ ÑÐ¸Ð¿Ñ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ, Ð² Ð¸Ñ ÑÐ¸ÑÐ»Ðµ Ð¼Ð¾Ð´Ð°Ð»ÑÐ½ÑÐ¹ ÑÐµÐ³ÑÐ»ÑÑÐ¾Ñ Ð´Ð»Ñ Ð´Ð¸ÑÐºÑÐµÑÐ½Ð¾Ð¹ Ð¸ Ð½ÐµÐ¿ÑÐµÑÑÐ²Ð½Ð¾Ð¹ ÑÐ¸ÑÑÐµÐ¼, ÑÐµÐ½ÑÑÐ°Ð»Ð¸Ð·Ð¾Ð²Ð°Ð½Ð½ÑÐ¹ ÑÐµÐ³ÑÐ»ÑÑÐ¾Ñ Ð¸ Ð´ÐµÑÐµÐ½ÑÑÐ°Ð»Ð¸Ð·Ð¾Ð²Ð°Ð½Ð½ÑÐ¹ ÑÐµÐ³ÑÐ»ÑÑÐ¾Ñ. ÐÐ¾ÑÐ»Ðµ ÑÑÐ¾Ð³Ð¾ Ð±ÑÐ»Ð¾ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¾ ÑÑÐ°Ð²Ð½ÐµÐ½Ð¸Ðµ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÑ ÑÐ¸Ð¿Ð¾Ð² ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÐ¼Ð¸ ÑÐ¿Ð¾ÑÐ¾Ð±Ð°Ð¼Ð¸, Ð½Ð°Ð¿ÑÐ¸Ð¼ÐµÑ ÑÑÐ°Ð²Ð½ÐµÐ½Ð¸Ðµ Ð¿Ð¾ Ð²ÐµÐºÑÐ¾ÑÐ½Ð¾Ð¼Ñ ÐºÑÐ¸ÑÐµÑÐ¸Ñ Ð¸ Ð²ÐµÑÐ±Ð°Ð»ÑÐ½Ð¾Ð¼Ñ Ð¼ÐµÑÐ¾Ð´Ñ Ð²ÑÐ±Ð¾ÑÐ° Ð½Ð°Ð¸Ð»ÑÑÑÐµÐ¹ Ð°Ð»ÑÑÐµÑÐ½Ð°ÑÐ¸Ð²Ñ. Ð¢Ð°Ðº Ð¶Ðµ Ð±ÑÐ»Ð¸ Ð¿Ð¾ÑÑÑÐ¾ÐµÐ½Ñ Ð³ÑÐ°ÑÐ¸ÐºÐ¸ Ð¿ÐµÑÐµÑÐ¾Ð´Ð½ÑÑ Ð¿ÑÐ¾ÑÐµÑÑÐ¾Ð² Ð¿Ð¾ ÐºÐ°Ð¶Ð´Ð¾Ð¼Ñ ÐºÐ¾Ð¼Ð¿Ð¾Ð½ÐµÐ½ÑÑ ÑÐ°Ð·Ð¾Ð²Ð¾Ð³Ð¾ Ð²ÐµÐºÑÐ¾ÑÐ°.
description: Object of research: a mathematical model of a helicopter of the MI-1 family. Subject of research: synthesis of various types of control of the longitudinal and lateral movement of a helicopter along a given trajectory. The purpose of the thesis is to investigate the behavior of a helicopter model when moving in the longitudinal and lateral planes using the MATLAB software tools. When performing work, you must perform: â¢ synthesis of various types of control; â¢ data visualization; â¢ analysis of the results obtained. As a result of the final qualification work, a helicopter model with an initial data set was considered. Various types of control have been synthesized, including a modal controller for discrete and continuous systems, a centralized controller, and a decentralized controller. This was followed by a comparison of different types of control in different ways, for example, comparison by vector criterion and the verbal method of choosing the best alternative. Also, graphs of transient processes were built for each component of the phase vector.