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The avionics handbook
- ISBN:084938348X
- Call Number : TL 695 .A8163 2001
- Title:The avionics handbook / edited by Cary R. Spitzer.
- Publisher:Boca Raton : CRC Press, 2001.
- Physical Description:1 v. (various pagings): ill.; 26 cm
- Series:The electrical engineering handbook series
- Notes:"Also in electronic format is available"
- Notes:Includes bibliographical references and index
- Subject:Avionics.
- Added Entry:Spitzer, Cary R.
The avionics handbook
- The Avionics Handbook
- Preface
- Biography
- Contributors
- Contents
- Section I Elements
- 1. AS 15531/MIL-STD- 1553B Digital Time Division Command/Response Multiplex Data Bus
- 1.1 Introduction
- 1.2 The Standard
- 1.3 Protocol
- 1.3.1 Word Types
- 1.3.2 Message Formats, Validation, and Timing
- 1.3.2.1 Bus Controller to Remote Terminal
- 1.3.2.2 Remote Terminal to Bus Controller
- 1.3.2.3 Remote Terminal to Remote Terminal
- 1.3.2.4 Mode Command Formats
- 1.3.2.5 Broadcast Information Transfer Formats
- 1.3.2.6 Command and Message Validation
- 1.3.2.7 Illegal Commands
- 1.3.2.8 Terminal Response Time
- 1.3.2.9 Intermessage Gap
- 1.3.2.10 Superseding Commands
- 1.3.3 Mode Codes
- 1.4 Systems-Level Issues
- 1.5 Testing
- Further Information
- 2. ARINC 429
- 2.1 Introduction
- 2.2 ARINC 419
- 2.3 ARINC 429
- 2.4 Message and Word Formatting
- 2.5 Timing-Related Elements
- 2.6 Communications Protocols
- 2.7 Applications
- 2.8 ARINC 453
- 3. Commercial Standard Digital Bus
- 3.1 Introduction
- 3.2 Bus Architecture
- 3.3 Basic Bus Operation
- 3.4 CSDB Bus Capacity
- 3.5 CSDB Error Detection and Correction
- 3.6 Bus User Monitoring
- 3.7 Integration Considerations
- 3.8 Bus Integration Guidelines
- 3.9 Bus Testing
- 3.10 Aircraft Implementations
- Defining Terms
- References
- Further Information
- Bibliography
- 4. Head-Up Displays
- 4.1 Introduction
- 4.2 HUD Fundamentals
- 4.3 Applications and Examples
- Defining Terms
- References
- 5. Head-Mounted Displays
- 6. Display Devices: RSD™ (Retinal Scanning Display)
- 7. Night Vision Goggles
- 7.1 Introduction
- 7.2 Fundamentals
- 7.3 Applications and Examples
- 7.3.1 Gen III and AN/AVS-6 ANVIS
- 7.3.2 Gen II and AN/PVS-5 NVG
- 7.3.3 Cat’s Eyes
- 7.3.4 NVG HUD
- 7.3.5 ANVIS HUD
- 7.3.6 Panoramic NVG
- 7.3.7 Low Profile NVG
- 7.3.8 Integrated Systems
- 7.3.9 Testing and Maintaining the NVG
- 7.3.10 Lighting Design Considerations
- 7.3.11 Types of Filters/Lighting Sources
- 7.3.12 Evaluating Aircraft Lighting
- 7.3.13 Measurement Equipment
- 7.3.14 Nighttime Illumination — Moon Phases
- 7.3.15 NVG in Civil Aviation
- References
- Further Information
- 8. Speech Recognition and Synthesis
- 8.1 Introduction
- 8.2 How Speech Recognition Works: A Simplistic View
- 8.3 Recent Applications
- 8.4 Flightdeck Applications
- Defining Terms
- References
- Bibliography
- Further Information
- 9. Human Factors Engineering and Flight Deck Design
- 10. Batteries
- 10.1 Introduction
- 10.2 General Principles
- 10.3 Lead-Acid Batteries
- 10.3.1 Theory of Operation
- 10.3.2 Cell Construction
- 10.3.3 Battery Construction
- 10.3.4 Discharge Performance
- 10.3.5 Charge Methods
- 10.3.6 Temperature Effects and Limitations
- 10.3.7 Service Life
- 10.3.8 Storage Characteristics
- 10.3.9 Maintenance Requirements
- 10.3.10 Failure Modes and Fault Detection
- 10.3.11 Disposal
- 10.4 Nickel-Cadmium Batteries
- 10.4.1 Theory of Operation
- 10.4.2 Cell Construction
- 10.4.3 Battery Construction
- 10.4.4 Discharge Performance
- 10.4.5 Charge Methods
- 10.4.6 Temperature Effects and Limitations
- 10.4.7 Service Life
- 10.4.8 Storage Characteristics
- 10.4.9 Maintenance Requirements
- 10.4.10 Failure Modes and Fault Detection
- 10.4.11 Disposal
- 10.5 Applications
- Defining Terms
- References
- Further Information
- 1. AS 15531/MIL-STD- 1553B Digital Time Division Command/Response Multiplex Data Bus
- SECTION II Functions
- 11. Boeing B-777: Fly-By- Wire Flight Controls
- 11.1 Introduction
- 11.2 System Overview
- 11.3 Design Philosophy
- 11.4 System Architecture
- 11.5 Control Surface Actuation
- 11.6 Fault Tolerance
- 11.7 System Operating Modes
- 11.8 Control Laws and System Functionality
- 11.9 Primary Flight Controls System Displays and Annunciations
- 11.10 System Maintenance
- 11.11 Summary
- Defining Terms
- 12. Electrical Flight Controls, From Airbus A320/330/340 to Future Military Transport Aircraft: A Fam...
- 13. Navigation Systems
- 14. Navigation and Tracking
- 15. Flight Management Systems
- 16. Synthetic Vision
- 17. Enhanced Situation Awareness
- 17.1 Enhanced Ground Proximity Warning System
- 17.2 Fundamentals of Terrain Avoidance Warning
- 17.3 Operating Modes
- 17.3.1 Mode 1 — Excessive Descent Rate
- 17.3.2 Mode 2 — Excessive Closure Rate
- 17.3.3 Mode 3 — Accelerating Flight Path Back into the Terrain after Take-off
- 17.3.4 Mode 4 — Unsafe Terrain Clearance Based on Aircraft Configuration
- 17.3.5 Mode 5 — Significant Descent Below the ILS Landing Glide Path Approach Aid
- 17.3.6 Mode 6 — Miscellaneous Callouts and Advisories
- 17.3.7 Mode 7 — Flight into Windshear Conditions
- 17.3.8 Envelope Modulation
- 17.3.9 “Enhanced Modes”
- 17.4 EGPWS Standards
- Further Information
- 18. TCAS II
- 11. Boeing B-777: Fly-By- Wire Flight Controls
- SECTION III Requirements, Design Analysis, Validation, and Certification
- 19. Setting Requirements
- 20.Digital Avionics Modeling and Simulation
- 21. Formal Methods
- 21.1 Introduction
- 21.2 Fundamentals of Formal Methods
- 21.3 Example Application
- 21.3.1 English Specification of the Example System
- 21.3.2 Formally Specifying the Example System
- 21.3.2.1 Events
- 21.3.2.2 State Description
- 21.3.2.3 Formal Specification of Nextstate Function
- 21.3.2.4 Specifying the att_cwsMode
- 21.3.2.5 Specifying the cas_eng Mode
- 21.3.2.6 Specifying the fpa_sel Mode
- 21.3.2.7 Specifying the alt_eng Mode
- 21.3.2.8 Input to Displays
- 21.3.2.9 Other Actions
- 21.3.2.10 Initial State
- 21.3.3 Formal Verification of the Example System
- 21.3.4 Alternative Methods of Specifying Requirements
- 21.3.1 English Specification of the Example System
- 21.4 Some Additional Observations
- Defining Terms
- References
- Further Information
- 22. Electronic Hardware Reliability
- 22.1 Introduction
- 22.2 Product Requirements and Constraints
- 22.3 The Product Life Cycle Environment
- 22.4 Characterization of Materials, Parts, and Manufacturing Processes
- 22.5 Parts Selection and Management
- 22.6 Failure Modes and Mechanisms
- 22.7 Design Guidelines and Techniques
- 22.8 Qualification and Accelerated Testing
- 22.9 Manufacturing Issues
- 22.10 Summary
- Defining Terms
- References
- Further Information
- 23. Certification of Civil Avionics
- 23.1 Introduction
- 23.2 Regulatory Basis of the Federal Aviation Administration
- 23.3 FAA Approvals of Avionics Equipment
- 23.4 FAA Designees
- 23.5 System Requirements
- 23.6 Safety Assessment
- 23.7 Environmental Qualification
- 23.8 Software Assurance
- 23.9 Manufacturing Approvals
- 23.10 The Joint Aviation Authorities
- 23.11 Summary
- Defining Terms
- Further Information
- 24. Processes for Engineering a System
- 24.1 Introduction
- 24.2 Structure of the Standard
- 24.3 Role of the EIA 632 Standard
- 24.4 Heritage of EIA 632
- 24.5 The Processes
- 24.6 Project Context
- 24.7 Key Concepts
- 24.7.1 The System and Its Products
- 24.7.2 Building Block Framework
- 24.7.3 Development of Enabling Products
- 24.7.4 Relationship Between the Building Blocks and the Processes
- 24.7.5 Hierarchy of Building Blocks
- 24.7.6 Requirements
- 24.7.7 Functional, Performance, and Interface Requirements
- 24.7.8 Verification and Validation
- Defining Terms
- References
- Further Information
- 25. Electromagnetic Environment (EME)
- SECTION IV Software
- 26. Ada
- 27. RTCA DO-178B/EUROCAE ED-12B
- SECTION V Implementation
- 28. Fault-Tolerant Avionics
- 28.1 Introduction
- 28.2 System Level Fault Tolerance
- 28.3 Hardware-Implemented Fault Tolerance (Fault-Tolerant Hardware Design Principles)
- 28.4 Software-Implemented Fault Tolerance—State Consistency
- 28.5 Software Fault Tolerance
- 28.6 Summary
- References
- Further Information
- 29. Boeing B-777
- 30. New Avionics Systems —Airbus A330/A340
- 31. McDonnell Douglas MD-11 Avionics System
- 31.1 Introduction
- 31.2 Flight Controls (ATA 22-00 and 27-00)
- 31.3 Communications System (ATA 23-00)
- 31.4 Entertainment System (23-00)
- 31.5 Display System (ATA 31-00)
- 31.6 Recording Systems (ATA 31-00)
- 31.7 Navigation Systems (ATA 34-00)
- 31.8 Maintenance Systems (ATA 45-00)
- 31.9 Aircraft Systems
- 31.10 Interchangeability
- 31.11 CNS/ATM Architecture
- 31.12 Derivatives
- 32. Lockheed F-22 Raptor
- 32.1 F-22 Role and Mission
- 32.2 IAS Hierarchical Functional Design
- 32.3 Integrated Avionics Architecture
- 32.4 Fault Tolerance and Recovery
- 32.5 Summary
- 33. Advanced Distributed Architectures
- 28. Fault-Tolerant Avionics