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當(dāng)前位置: 首頁(yè)出版圖書科學(xué)技術(shù)航空、航天航空現(xiàn)代航空發(fā)動(dòng)機(jī)多變量控制系統(tǒng):英文版

現(xiàn)代航空發(fā)動(dòng)機(jī)多變量控制系統(tǒng):英文版

現(xiàn)代航空發(fā)動(dòng)機(jī)多變量控制系統(tǒng):英文版

定 價(jià):¥61.00

作 者: 孫健國(guó)主編
出版社: 北京航空航天大學(xué)出版社
叢編項(xiàng):
標(biāo) 簽: 交通運(yùn)輸

ISBN: 9787810775908 出版時(shí)間: 2005-10-01 包裝: 膠版紙
開本: 20cm 頁(yè)數(shù): 621 字?jǐn)?shù):  

內(nèi)容簡(jiǎn)介

  Inthisbookthemethodologyandconceptofdesigningmultivariablecontrolsystemsforaeroenginesarepresentedwhichinclude:generaldevelopmenttendenciesinaeroenginesandaeroenginecontrolsystems;modelingofaeroengines;designofvariouscontrollawsforaeroengines;designoffaulttolelantcontrolsystemsforaeroenginesanddesignofintegratedflight/propulsioncontrolsystems.<br>Thisbookisusefultopracticingengineersanddesignersofaeroenginecontrolsystemsandaeroenginesasareferencebookandasanupdatedtotheirengineeringeducation.ThisbookshouldproveusefulalsoforPhDandMSccandidatesofdisciplinesofaeroenginecontrolsystemsandaeroenginesfortheirgraduatecourses.<br>本書闡述現(xiàn)代航空發(fā)動(dòng)機(jī)多變量控制系統(tǒng)設(shè)計(jì)方法及概念:航空發(fā)動(dòng)機(jī)及其控制系統(tǒng)的發(fā)展趨勢(shì);航空發(fā)動(dòng)機(jī)建模;各種航空發(fā)動(dòng)機(jī)現(xiàn)代控制規(guī)律的設(shè)計(jì);發(fā)動(dòng)機(jī)容錯(cuò)控制系統(tǒng)設(shè)計(jì)以及飛行/推進(jìn)綜合控制系統(tǒng)設(shè)計(jì)。<br>本書可作為航空發(fā)動(dòng)機(jī)控制和航空發(fā)動(dòng)機(jī)總體專業(yè)工程技術(shù)人員的參考書,也可作為上述專業(yè)的研究生教材。<br>

作者簡(jiǎn)介

暫缺《現(xiàn)代航空發(fā)動(dòng)機(jī)多變量控制系統(tǒng):英文版》作者簡(jiǎn)介

圖書目錄

Chapter 1 State of the Art and Problems of the Development of Aeroengines and Their Control Systems
1.1 System Approach to the Development of Complex Technical Systems
1.2 Tendencies of the Aeroengine Development
1.3 Tendencies of the Development of Production and Technolo gical Systems
1.4 Tendencies of the Aeroengine Control System Development
1.5 System Conception of Designing Aeroengine Control Systems
References57
Chapter 2 Modeling of Aeroengines
2.1 Introduction
2.2 Component Level Model
2.2.1 Inlet
2.2.2 Fan
2.2.3 Compressor
2.2.4 Engine Bleeds
2.2.5 Turbines
2.2.6 Main Combustor
2.2.7 Augmentor
2.2.8 Bypass Duct
2.2.9 Exhaust Nozzle
2.2.10 Engine Dynamics78
2.2.11 Remarks83
2.3 State Variable Mode
2.3.1 Partial Derivative Method
2.3.2 Fitting Metbod
2.3.3 Remarks
2.3.4 Simulation Results
2.4 Adaptive Model
2.4.1 Adaptive Model Estimating Unmeasured Outputs
2.4.2 Component Tracking Filter
2.5 Intelligent Model
2.5.1 Modeling by Neural Network
2.5.2 Modeling with Genetic Algorithm
2.6 Estimator of Aeroengine Performance Parameters
2.6.1 Introduction
2.6.2 Model Based Control
2.6.3 Estimator Based Control
References
Chapter 3 Adaptive Control Systems of Aeroengines
3.1 Introduction
3.2 The Main Types of Adaptive Systems
3.3 The Structure of Multivariable MRAC Systems
3.3.1 Design of Generalized Tuned Plant
3.3.2 Self Tuning Algorithms
3.4 Linearized Model of Multivariable MRAC Systems
3.5 Design of Multivariable MRAC Systems
3.5.1 Design of the Coupled Correcting Device
3.5.2 Design of Non Coupled Correcting Device
3.6 Non Linear Correction of Self Tuning Algorithms
3.7 Structural Features of Multivariable MRAC Systems for Aeroengines
3.8 Design of Linearized Model of Multivariable MRAC Systems in the State Space
References
Chapter 4 Extremal Control System of Turbo Prop Fan Engines
……
Chapter 5 Intelligent Control Systems of Aeroengines
Chapter 6 Multivariable Robust Control Systems of Aeroengines
Chapter 7 Fault Tolerant Digital Control Systems of Aeroengines
Chapter 8 Integrated Flight/Propulsion Control System
References

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