何晓薇、向淑兰编著的《航空电子设备(飞行技术专业系列教材)(英文版)》是根据中国民般飞行学院1995年制定的“航空电子设备教学大纲”编写而成的。该教材较为系统地阐述了现代民般运输机电了设备的基本理论和知识，主要作为飞行技术专业学业习“航空电子设备”课程的教材；同时，也可供其他相关人员学习、参考。

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 Instruments

Chapter 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 Monitoring

Chapter 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 Typical Auto Flight Operation for B767 Airplane

Chapter 4 Flight Data Recording & Airplane Condition Monitoring System

 4.1 Introduction

 4.2 Flight Data Recording System

 4.3 Airplane Condition Monitoring System

Chapter 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 Warning

Chapter 6 Secondary Surveillance Radar and Transponder

 6.1 Introduction

 6.2 Air Traffic Control Radar Beacon System

 6.3 Mode S Secondary Radar System

Chapter 7 Traffic Alert and Collision Avoidance System

 7.1 Introduction

 7.2 TCAS II System Architecture

 7.3 The Principle of Operation ofTCAS II

 7.4 TCAS II Displays

 7.5 TCAS IIAural Messages

 7.6 Control Panel

 7.7 Crew Response

 7.8 The Use ofTCAS II

 7.9 Flight Crew Procedure for A320 Airplane

Chapter 8 Ground Proximity Warning System

 8.1 Introduction

 8.2 GPWS System Architecture

 8.3 GPWSAlert Modes

Chapter 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 Procedures

Chapter 10 Runway Awareness and Advisory System

 10.1 Introduction

 10.2 The Principle of RAAS

 10.3 System Operation Description

 10.4 RAAS Quick Reference

Chapter 11 Predictive Windshear System

 11.1 Introduction

 11.2 The Principle of PWS

 II.3 Limitations of PWS

 11.4 The Alert of PWS

 11.5 The Operation of PWS

 11.6 Flight Crew Procedure for A320 Airplane

Chapter 12 Radio Altimeter

 12.1 Introduction

 12.2 The Principle of LRRA

 12.3 Radio Altitude Display

 12.4 Errors and Accuracy

Chapter 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 CDU

Chapter 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 Alignment

Chapter 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 GPS

Chapter 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 Operation

References