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

內(nèi)容概要

本書(shū)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)。     本書(shū)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(zhuān)業(yè)工程技術(shù)人員的參考書(shū)，也可作為上述專(zhuān)業(yè)的研究生教材。

書(shū)籍目錄

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  References57Chapter 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  ReferencesChapter 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 AeroenginesChapter 6 Multivariable Robust Control Systems of AeroenginesChapter 7 Fault Tolerant Digital Control Systems of AeroenginesChapter 8 Integrated Flight/Propulsion Control SystemReferences

編輯推薦

《Advanced Multivariable Control Systems of Aeroengines》由北京航天航空大學(xué)出版社出版，In this book the methodology and concept of designing multivariable control systems for aeroengines are presented which include: general development tendencies in aeroengines and aeroengine control systems; modeling of aeroengines; design of various control laws for aeroengines; design of fault tolelant control systems for aeroengines and design of integrated flight/propulsion control systems. This book is useful to practicing engineers and designers of aeroengine control systems and aeroengines as a reference book and as an updated to their engineering education. This book should prove useful also for PhD and MSc candidates of disciplines of aeroengine control systems and aeroengines for their graduate courses.

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