Mechanical Structure Design of the Aircraft ASD Control Isolation Control

Aircraft control system is of key importance for flight attitude control of aircrafts. Its normal function directly determines whether the aircraft flies safely, flight delay, and dispatch reliability. Therefore, this paper designs the mechanical structure of the aircraft ASD control isolation contr...

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Main Authors: Qiongyan Shi, Jianghua Zhang
Format: Article
Language:English
Published: Wiley 2022-01-01
Series:Journal of Applied Mathematics
Online Access:http://dx.doi.org/10.1155/2022/8306216
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author Qiongyan Shi
Jianghua Zhang
author_facet Qiongyan Shi
Jianghua Zhang
author_sort Qiongyan Shi
collection DOAJ
description Aircraft control system is of key importance for flight attitude control of aircrafts. Its normal function directly determines whether the aircraft flies safely, flight delay, and dispatch reliability. Therefore, this paper designs the mechanical structure of the aircraft ASD control isolation control. Firstly, the mechanical control principle of the driving rod system is analyzed, and the isolation mechanism of pitch and roll control is designed; secondly, the control lines are classified, the transmission characteristic requirements of the aircraft control isolation system are given, the transmission ratio distribution and calculation of the aircraft control isolation system are given, and finally, the mechanism design of the aircraft ASD control isolation system is realized.
format Article
id doaj-art-2de22e1e59fe42a4bb19a102ca57ae73
institution Kabale University
issn 1687-0042
language English
publishDate 2022-01-01
publisher Wiley
record_format Article
series Journal of Applied Mathematics
spelling doaj-art-2de22e1e59fe42a4bb19a102ca57ae732025-08-20T03:55:07ZengWileyJournal of Applied Mathematics1687-00422022-01-01202210.1155/2022/8306216Mechanical Structure Design of the Aircraft ASD Control Isolation ControlQiongyan Shi0Jianghua Zhang1College of Mechanical EngineeringCollege of Mechanical EngineeringAircraft control system is of key importance for flight attitude control of aircrafts. Its normal function directly determines whether the aircraft flies safely, flight delay, and dispatch reliability. Therefore, this paper designs the mechanical structure of the aircraft ASD control isolation control. Firstly, the mechanical control principle of the driving rod system is analyzed, and the isolation mechanism of pitch and roll control is designed; secondly, the control lines are classified, the transmission characteristic requirements of the aircraft control isolation system are given, the transmission ratio distribution and calculation of the aircraft control isolation system are given, and finally, the mechanism design of the aircraft ASD control isolation system is realized.http://dx.doi.org/10.1155/2022/8306216
spellingShingle Qiongyan Shi
Jianghua Zhang
Mechanical Structure Design of the Aircraft ASD Control Isolation Control
Journal of Applied Mathematics
title Mechanical Structure Design of the Aircraft ASD Control Isolation Control
title_full Mechanical Structure Design of the Aircraft ASD Control Isolation Control
title_fullStr Mechanical Structure Design of the Aircraft ASD Control Isolation Control
title_full_unstemmed Mechanical Structure Design of the Aircraft ASD Control Isolation Control
title_short Mechanical Structure Design of the Aircraft ASD Control Isolation Control
title_sort mechanical structure design of the aircraft asd control isolation control
url http://dx.doi.org/10.1155/2022/8306216
work_keys_str_mv AT qiongyanshi mechanicalstructuredesignoftheaircraftasdcontrolisolationcontrol
AT jianghuazhang mechanicalstructuredesignoftheaircraftasdcontrolisolationcontrol