Experimental Model-Based Aeroelastic Control for Flutter Suppression and Gust-Load Alleviation

被引：16

作者：

Zeng, Jie ^{[1
]}

Kukreja, Sunil L. ^{[2
]}

Moulin, Boris ^{[3
]}

机构：

[1] ZONA Technol Inc, Res & Dev Control Syst, Scottsdale, AZ 85258 USA

[2] NASA Dryden Flight Res Ctr, Edwards AFB, CA 93523 USA

[3] ZONA Technol Inc, Scottsdale, AZ 85258 USA

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2012年 / 35卷 / 05期

关键词：

D O I：

10.2514/1.56790

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper introduces an experimental model-based feedback-control framework for flutter suppression and gust load alleviation. With the proposed experimental model-based feedback-control framework, the flexible dynamics can be consistently estimated via system-identification algorithms, and its undesirable effects are suppressed through a robust feedback-control law while the whole system's stability is being maintained. Therefore, the resilience of the flight control law in the presence of aeroelastic/aeroservoelastic interactions can be increased by the suppression of the aircraft's structural vibrations induced by the flutter mechanism and/or gust perturbation. The proposed experimental model-based feedback-control technique is demonstrated on the SuperSonic SemiSpan Transport wind-tunnel model for flutter suppression and gust-load alleviation.

引用

页码：1377 / 1390

页数：14

共 50 条

[41] Iterative Learning Control of a Nonlinear Aeroelastic System despite Gust Load
Xu, Xing-zhi
Gao, Ya-kui
Zhang, Wei-guo
[J]. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2015, 2015
[42] Toward Automated Gust Load Alleviation Control Design via Discrete Gust Impulse Filters
Cavaliere, Davide
Fezans, Nicolas
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2024, 47 (04) : 697 - 710
[43] Gust load alleviation design for MUPAL-α experimental aircraft based on the panel method estimation
Kouda, K
Matsushita, H
[J]. SICE 2003 ANNUAL CONFERENCE, VOLS 1-3, 2003, : 924 - 929
[44] Application of Model-following Adaptive Neural Network Control Theory in Gust Load Alleviation
Nie, Rui
Zhang, Weiguo
Li, Guangwen
Liu, Xiaoxiong
[J]. 2009 IEEE INTERNATIONAL CONFERENCE ON AUTOMATION AND LOGISTICS ( ICAL 2009), VOLS 1-3, 2009, : 389 - 393
[45] Airfoil gust load alleviation based on dual synthetic jets
Wang, Hao
Luo, Zhenbing
Deng, Xiong
Zhou, Yan
Zhang, Jianyuan
Zhao, Zhijie
[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2024, 45 (16):
[46] Flutter Suppression of Nonlinear Aeroelastic System using Adaptive Control based on Neural Network
Tan, Puxue
Li, Daochun
Kan, Zi
Tian, Maojiang
Xiang, Jinwu
[J]. 2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2018,
[47] Gust load alleviation on an aircraft wing by trailing edge Circulation Control
Li, Yonghong
Qin, Ning
[J]. JOURNAL OF FLUIDS AND STRUCTURES, 2021, 107
[48] Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation
Balatti, Davide
Khodaparast, Hamed Haddad
Friswell, Michael I.
Manolesos, Marinos
Castrichini, Andrea
[J]. JOURNAL OF FLUIDS AND STRUCTURES, 2023, 119
[49] Active suppression of flutter and gust response of bridge using edge control surfaces
Kwon, SD
Chang, SP
Kim, YS
[J]. WIND ENGINEERING INTO THE 21ST CENTURY, VOLS 1-3, 1999, : 941 - 946
[50] ACTIVE CONTROL OF ORIGAMI INSPIRED CAMBER MORPHING AIRFOIL FOR GUST LOAD ALLEVIATION
Magar, Kaman Thapa
Fuchi, Kazuko
Pankonien, Alexander M.
Beblo, Richard V.
Reich, Gregory W.
[J]. PROCEEDINGS OF THE ASME CONFERENCE ON SMART MATERIALS, ADAPTIVE STRUCTURES AND INTELLIGENT SYSTEMS, 2018, VOL 1, 2018,

← 1 2 3 4 5 →