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检索条件"主题词=Benchmark Active Control Technology"
37 条 记 录,以下是1-10 订阅
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active Flutter Suppression: Quantification of Performance Loss Due to Actuator Saturation
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JOURNAL OF GUIDANCE control AND DYNAMICS 2024年 第11期47卷 2333-2350页
作者: Micheli, Boris German Aerosp Ctr DLR Inst Aeroelast Dept Aeroelast Simulat Bunsenstr 10 D-37073 Gottingen Germany
active flutter suppression technologies have the potential to lead to major weight savings while keeping the envisaged flight envelope for the future generation of commercial aircraft. Since the stabilization of aeroe... 详细信息
来源: 评论
Predictive Cost Adaptive control of the BACT Flutter Model
Predictive Cost Adaptive Control of the BACT Flutter Model
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AIAA SciTech Forum
作者: Richards, Riley J. Islam, S. A. U. Bernstein, Dennis S. Univ Michigan Dept Aerosp Engn Ann Arbor MI 48109 USA
This paper provides a numerical investigation of the performance of predictive cost adaptive control (PCAC) of the NASA BACT flutter model. PCAC is an indirect adaptive control extension of model predictive control th... 详细信息
来源: 评论
Composite Adaptive Aeroelastic System control and Multifold Regressor Integrals-based Identification
Composite Adaptive Aeroelastic System Control and Multifold ...
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AIAA Aviation Forum
作者: Lee, Keum W. Rajt, Kaushik Singh, Sahjendra N. Catholic Kwandong Univ Dept Elect Engn Gangwon 25601 South Korea Univ Nevada Las Vegas Dept Elect & Comp Engn Las Vegas NV 89154 USA
The paper presents a composite adaptive control system for the stabilization and parameter estimation of a multi-input multi-output two degree of freedom aeroelastic system equipped with leading- and trailing-edge con... 详细信息
来源: 评论
Data-Driven Retrospective Cost Adaptive control for Flight control Applications
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JOURNAL OF GUIDANCE control AND DYNAMICS 2021年 第10期44卷 1732-1758页
作者: Ul Islam, Syed Aseem Nguyen, Tam W. Kolmanovsky, Ilya, V Bernstein, Dennis S. Univ Michigan Aerosp Engn 1320 Beal Ave Ann Arbor MI 48109 USA
Unlike fixed-gain robust control, which trades off performance with modeling uncertainty, direct adaptive control uses partial modeling information for online tuning. The present paper combines retrospective cost adap... 详细信息
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Discrete Time State Space Modeling for Gust Aerodynamics with Component Load Monitoring
Discrete Time State Space Modeling for Gust Aerodynamics wit...
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AIAA Science and technology Forum and Exposition (AIAA SciTech Forum)
作者: Wang, Z. Sarhaddi, D. Chen, P. C. ZONA Technol Inc Scottsdale AZ 85258 USA
In this paper, we extend our previous work on the discrete time state space aeroelastic modeling technique using FUN3D further for the gust analysis. We have utilized a subspace realization algorithm to identify the i... 详细信息
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Experimental Nonlinear control for Flutter Suppression in a Nonlinear Aeroelastic System
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JOURNAL OF GUIDANCE control AND DYNAMICS 2017年 第8期40卷 1925-1938页
作者: Jiffri, Shakir Fichera, Sebastiano Mottershead, John E. Da Ronch, Andrea Univ Liverpool Dept Mech Mat & Aerosp Engn Sch Engn Brownlow Hill Liverpool L69 3GH Merseyside England Univ Liverpool Appl Mech Brownlow Hill Liverpool L69 3GH Merseyside England Univ Liverpool Inst Risk & Uncertainty Brownlow Hill Liverpool L69 3GH Merseyside England Univ Southampton Fac Engn & Environm Univ Rd Southampton SO17 1BJ Hants England
Experimental implementation of input-output feedback linearization in controlling the dynamics of a nonlinear pitch-plunge aeroelastic system is presented. The control objective is to linearize the system dynamics and... 详细信息
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Design of an active Disturbance Rejection control for Transonic Flutter Suppression
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JOURNAL OF GUIDANCE control AND DYNAMICS 2017年 第11期40卷 2905-2916页
作者: Yang, Zhijun Huang, Rui Zhao, Yonghui Hu, Haiyan Nanjing Univ Aeronaut & Astronaut State Key Lab Mech & Control Mech Struct Inst Vibrat Engn Res Nanjing 210016 Jiangsu Peoples R China
Conventional controls, such as an optimal control with a notch filter, are able to remove the flutter instability under subsonic flows but may need higher adaptability to make the controllers stable under transonic fl... 详细信息
来源: 评论
Flutter Suppression for Underactuated Aeroelastic Wing Section: Nonlinear Gain-Scheduling Approach
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JOURNAL OF GUIDANCE control AND DYNAMICS 2017年 第8期40卷 2102-2109页
作者: Lhachemi, H. Chu, Y. Saussie, D. Zhu, G. Ecole Polytech Montreal Dept Elect Engn Montreal PQ H3T 1J4 Canada
Presented as Paper 2017-1735 at the AIAA Guidance, Navigation, and control Conference, Grapevine, TX, 9-13 January 2017
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Wind-Tunnel Tests for active Flutter control and Closed-Loop Flutter Identification
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AIAA JOURNAL 2016年 第7期54卷 2089-2099页
作者: Huang, Rui Zhao, Yonghui Hu, Haiyan Nanjing Univ Aeronaut & Astronaut Inst Vibrat Engn Res State Key Lab Mech & Control Mech Struct Nanjing 210016 Jiangsu Peoples R China
In this study, active flutter control and closed-loop flutter identification were experimentally studied for a low-aspect-ratio wing model in an Nanhang-2 subsonic wind tunnel. To actively suppress the flutter of the ... 详细信息
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Output Regulation with Actuator Saturation for the benchmark active control technology Model
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JOURNAL OF GUIDANCE control AND DYNAMICS 2010年 第6期33卷 1951-1966页
作者: Applebaum, Ellen Adin, Zvi J. Ben-Asher, Joseph Z. Technion Israel Inst Technol Fac Aerosp Engn IL-32000 Haifa Israel
A study was conducted to address the problem of output regulation of the continuous-time linear benchmark active control technology (BACT) model with control saturation and exogenous input additive disturbance. The BA... 详细信息
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