Aerodynamic analysis and elastic suppression of refueling boom

This paper studies on the refueling boom aerodynamic characteristics and proposes an elastic suppression method for the refueling boom with the property of large length-diameter ratio. In order to obtain the accurate frequency response, modal analysis for the refueling boom is conducted based on ANS...

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Main Authors: Qu Yaohong, Mu Xue, Wang Zhuoya, Xiao Bing
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:MATEC Web of Conferences
Subjects:
Online Access:https://doi.org/10.1051/matecconf/201713900058
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author Qu Yaohong
Mu Xue
Wang Zhuoya
Xiao Bing
author_facet Qu Yaohong
Mu Xue
Wang Zhuoya
Xiao Bing
author_sort Qu Yaohong
collection DOAJ
description This paper studies on the refueling boom aerodynamic characteristics and proposes an elastic suppression method for the refueling boom with the property of large length-diameter ratio. In order to obtain the accurate frequency response, modal analysis for the refueling boom is conducted based on ANSYS MODAL. Then the dynamics and kinematic equations of the elastic refueling boom are deduced, which contain the frequency parameter. To complete the equations, the aerodynamic performance is solved in ANSYS FLUENT. In addition, based on the mixed H2 / H∞ theory, an optimal PID controller is proposed to suppress the elastic deformation. Furthermore, the parameters of the PID controller are optimized with the differential evolution algorithm. Simulation shows that the different elastic mode has different effect on the control of the refueling boom. The elastic deformation is suppressed obviously for each mode.
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spelling doaj.art-37d90f89dd7842149a1333f931c199b22022-12-21T22:04:45ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011390005810.1051/matecconf/201713900058matecconf_icmite2017_00058Aerodynamic analysis and elastic suppression of refueling boomQu YaohongMu XueWang ZhuoyaXiao BingThis paper studies on the refueling boom aerodynamic characteristics and proposes an elastic suppression method for the refueling boom with the property of large length-diameter ratio. In order to obtain the accurate frequency response, modal analysis for the refueling boom is conducted based on ANSYS MODAL. Then the dynamics and kinematic equations of the elastic refueling boom are deduced, which contain the frequency parameter. To complete the equations, the aerodynamic performance is solved in ANSYS FLUENT. In addition, based on the mixed H2 / H∞ theory, an optimal PID controller is proposed to suppress the elastic deformation. Furthermore, the parameters of the PID controller are optimized with the differential evolution algorithm. Simulation shows that the different elastic mode has different effect on the control of the refueling boom. The elastic deformation is suppressed obviously for each mode.https://doi.org/10.1051/matecconf/201713900058refueling boom;aerodynamic analysis;modal analysis;elastic suppression;mixed optimal PID controller
spellingShingle Qu Yaohong
Mu Xue
Wang Zhuoya
Xiao Bing
Aerodynamic analysis and elastic suppression of refueling boom
MATEC Web of Conferences
refueling boom;
aerodynamic analysis;
modal analysis;
elastic suppression;
mixed optimal PID controller
title Aerodynamic analysis and elastic suppression of refueling boom
title_full Aerodynamic analysis and elastic suppression of refueling boom
title_fullStr Aerodynamic analysis and elastic suppression of refueling boom
title_full_unstemmed Aerodynamic analysis and elastic suppression of refueling boom
title_short Aerodynamic analysis and elastic suppression of refueling boom
title_sort aerodynamic analysis and elastic suppression of refueling boom
topic refueling boom;
aerodynamic analysis;
modal analysis;
elastic suppression;
mixed optimal PID controller
url https://doi.org/10.1051/matecconf/201713900058
work_keys_str_mv AT quyaohong aerodynamicanalysisandelasticsuppressionofrefuelingboom
AT muxue aerodynamicanalysisandelasticsuppressionofrefuelingboom
AT wangzhuoya aerodynamicanalysisandelasticsuppressionofrefuelingboom
AT xiaobing aerodynamicanalysisandelasticsuppressionofrefuelingboom