《现代航空发动机多变量控制系统》阐述现代航空发动机多变量控制系统设计方法及概念：航空发动机及其控制系统的发展趋势；航空发动机建模；各种航空发动机现代控制规律的设计；发动机容错控制系统设计以及飞行/推进综合控制系统设计。 《现代航空发动机多变量控制系统》可作为航空发动机控制和航空发动机总体专业工程技术人员的参考书，也可作为上述专业的研究生教材。
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
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