何晓薇、向淑兰主编的《航空电子设备(第2版飞行技术专业系列教材)(英文版)》是航空电子设备英文版，系统介绍了民航当前采用的通信、导航、仪表及自动控制系统的种类、功能和工作原理，包括：高频通信、甚高频通信等常见机载通信设备的原理、结构、使用方法，导航设备(VOR、DME、ILS和ADF) 、雷达系统及机载监视设备(TCAS、GPWS和风切变探测系统)等的原理与使用方法，航空仪表的基础知识和飞机的基本仪表设备，自动飞行控制系统的作用、组成、控制规律等。

Chapter 1 Air Data Computer System 1. 1 Introduction 1.2 The Basic Principle 1.3 Temperature Measurement Probes 1.4 Pressure Transducers 1.5 Air Data InstrumentsChapter 2 Electronic Instrument Systems 2.1 Introduction 2.2 Electronic Flight Instrument Systems 2.3 Engine Indicating and Crew Alerting System 2.4 Electronic Centralized Aircraft MonitoringChapter 3 Automatic Flight Control Systems 3.1 Introduction 3.2 The Flight Director 3.3 The Autopilot 3.4 Autopilot Flight Director Systems 3.5 The Yaw Damper 3.6 Automatic Pitch Trim 3.7 Autothrottle 3.8 Autoland 3.9 Flight Envelope Protection 3.10 Typical Auto Flight Operation for B767 AirplaneChapter 4 Flight Data Recording & Airplane Condition Monitoring System 4.1 Introduction 4.2 Flight Data Recording System 4.3 Airplane Condition Monitoring SystemChapter 5 Airborne Weather Radar System 5.1 Introduction 5.2 Basic Principles 5.3 Control Panel 5.4 Display-EHSI Presentation 5.5 Operation In-Flight 5.6 WarningChapter 6 Secondary Surveillance Radar and Transponder 6.1 Introduction 6.2 Air Traffic Control Radar Beacon System 6.3 Mode S Secondary Radar SystemChapter 7 Traffic Alert and Collision Avoidance System 7.1 Introduction 7.2 TCAS II System Architecture 7.3 The Principle of Operation of TCAS II 7.4 TCAS II Displays 7.5 TCAS II Aural Messages 7.6 Control Panel 7.7 Crew Response 7.8 The Use of TCAS II 7.9 Flight Crew Procedure for A320 AirplaneChapter 8 Ground Proximity Warning System 8.1 Introduction 8.2 GPWS System Architecture 8.3 GPWS Alert ModesChapter 9 Enhanced Ground Proximity Warning System 9.1 Introduction 9.2 Enhanced GPWS Features 9.3 Look-Ahead Terrain Alerting 9.4 Terrain Display 9.5 Flight Deck Effects for EGPWS Alert 9.6 Aural Message Priority 9.7 EGPWS Control Panel 9.8 Flight Crew ProceduresChapter 10 Runway Awareness and Advisory System 10.1 Introduction 10.2 The Principle of RAAS 10.3 System Operation Description 10.4 RAAS Quick ReferenceChapter 11 Predictive Windshear System 11.1 Introduction 11.2 The Principle of PWS 11.3 Limitations of PWS 11.4 The Alert of PWS 11.5 The Operation of PWS 11.6 Flight Crew Procedure for A320 AirplaneChapter 12 Radio Altimeter 12.1 Introduction 12.2 The Principle of LRRA 12.3 Radio Altitude Display 12.4 Errors and AccuracyChapter 13 Inertial Navigation System 13.1 Introduction 13.2 The Principle and Construction of the Accelerometer 13.3 The Gyro-Stabilised (Gimballed) Platform 13.4 Position Calculation 13.5 INS Self-Alignment 13.6 INS Error Corrections 13.7 Mode Selector Panel and CDUChapter 14 Inertial Reference System 14.1 Description of the Strapdown System 14.2 The Control and Display oflRS 14.3 The IRS Outputs 14.4 IRS AlignmentChapter 15 Global Positioning System 15.1 Introduction 15.2 GPS Elements 15.3 GPS Operating Principle 15.4 GPS Receiver Unit 15.5 GPS Reliability/Integrity 15.6 GPS Errors 15.7 Differential GPSChapter 16 Flight Management Computer System 16.1 Introduction 16.2 FMCS Architecture 16.3 Command Display Unit 16.4 The Flight Management Computer Database 16.5 General FMS OperationReferences