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Titlebook: Aeroservoelasticity; Modeling and Control Ashish Tewari Book 2015 Springer Science+Business Media, LLC 2015 active load alleviation and flu

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发表于 2025-3-21 19:05:14 | 显示全部楼层 |阅读模式
期刊全称Aeroservoelasticity
期刊简称Modeling and Control
影响因子2023Ashish Tewari
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发行地址First book on aeroservoelastic modeling and analysis.Presents aeroservoelasticity in the modern controls context by multivariable, state-space methods including robust, nonlinear, and adaptive control
学科分类Control Engineering
图书封面Titlebook: Aeroservoelasticity; Modeling and Control Ashish Tewari Book 2015 Springer Science+Business Media, LLC 2015 active load alleviation and flu
影响因子.This monograph presents the state of the art in aeroservoelastic (ASE) modeling and analysis and develops a systematic theoretical and computational framework for use by researchers and practicing engineers. It is the first book to focus on the mathematical modeling of structural dynamics, unsteady aerodynamics, and control systems to evolve a generic procedure to be applied for ASE synthesis. Existing robust, nonlinear, and adaptive control methodology is applied and extended to some interesting ASE problems, such as transonic flutter and buffet, post-stall buffet and maneuvers, and flapping flexible wing..The author derives a general aeroservoelastic plant via the finite-element structural dynamic model, unsteady aerodynamic models for various regimes in the frequency domain, and the associated state-space model by rational function approximations. For more advanced models, the full-potential, Euler, and Navier-Stokes methods for treating transonic and separated flows are also briefly addressed. Essential ASE controller design and analysis techniques are introduced to the reader, and an introduction to robust control-law design methods of LQG/LTR and H2/H∞ synthesis is followed
Pindex Book 2015
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Aeroservoelasticity978-1-4939-2368-7Series ISSN 2373-7719 Series E-ISSN 2373-7727
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Ashish TewariFirst book on aeroservoelastic modeling and analysis.Presents aeroservoelasticity in the modern controls context by multivariable, state-space methods including robust, nonlinear, and adaptive control
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Hahn-Banach extension theorems,oduction on assumptions and idealizations required for modeling aircraft structures, the principles of static load-displacement relations, flexibility influence coefficients, virtual work, strain energy, and stiffness influence coefficients are described. For the dynamic case, the structural dynamic
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https://doi.org/10.1007/978-0-387-72743-1ear operational relationship between pressure distribution and upwash distribution on a lifting surface for subsonic and supersonic flows, and a nonlinear partial differential equation (Euler, full-potential, or transonic small-disturbance equation) for transonic flows. The treatment of the flow mod
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