Policy on Intellectual Property Right (IPR)
1 Introduction
2 Discussion
2.1 Substitution
of wiring
2.2 Enhanced
reliability
2.3 Additional
functions
3 Wireless Avionics
Intra-Communications application characteristics
3.1 Categorization
process description
3.1.1 System
data rate categorization
3.1.2 System
location
3.1.3 Category
definition
3.2 Detailed
description of applications by category
3.2.1 Category
low data rate inside
3.2.2 Category
low data rate outside
3.2.3 Category
High data rate Inside
3.2.4 Category
High data rate Outside
4 Wireless Avionics
Intra-Communications system characteristics
4.1 Reference
aircraft
4.2 Reference
Wireless Avionics Intra-Communications (WAIC) system architecture
4.2.1 Network
components
4.2.2 Generic
network architecture for internal Wireless Avionics Intra-Communications
applications (low and high data rate inside)
4.2.3 Generic
network architecture for external Wireless Avionics Intra-Communications
applications (low and high data rate outside)
4.3 Aircraft
shielding characteristics
4.3.1 Wireless
Avionics Intra-Communications systems inside the aircraft structure
4.4 Wireless
Avionics Intra-Communications radio interface characteristics
4.5
Overall effective radiated power per aircraft
and Wireless Avionics Intra‑Communications application category
5 Spectrum requirements for
Wireless Avionics Intra-Communications
5.1 Net average
application data rate (Peff)
5.2 Protocol
overhead factor (a)
5.3 Channelization
overhead factor (b)
5.4 Multiple
aircraft factor
5.5 Modulation
efficiency
5.6 Calculation of
Wireless Avionics Intra-Communications spectrum requirements
6 Summary
Annex 1 Protocol considerations
A-1.1 Introduction
A-1.2 Overhead in
IEEE 802.15.4 and 802.11a/g packed-oriented communications systems
A-1.3 Security-related
overhead
A-1.4 Error
correction overhead
A-1.5 Calculation of
protocol overhead factor a
A-1.6 Channelization
overhead factor b
A-1.7 Modulation
efficiency η
Annex 2 Multiple aircraft considerations
A-2.1 Aircraft-to-aircraft
interference model
A-2.2 Aircraft model
A-2.3 Distribution
of Wireless Avionics Intra-Communications nodes outside the aircraft structure
A-2.4 Interference
ranges
A-2.5 Aircraft
configuration
A-2.6 Estimated
number of interfering aircraft
A-2.7 Multiplicative
factor for spectrum requirements
A-2.8 Conclusion on
multiple aircraft overhead
Annex 3 Propagation considerations
A-3.1 Introduction
A-3.2 Definition of
channel gain/loss models for various areas of the aircraft
A-3.3 General
channel model
A-3.4 Modelling
large-scale channel characteristics
A-3.5 Large-scale
prediction error or modelling shadowing
A-3.6 Modelling
small-scale fading statistics
A-3.7 Modelling
aircraft fuselage attenuation in closed form
Annex 4 Overall emissions of an aircraft caused by
Wireless Avionics Intra-Communications systems
A-4.1 Introduction
A-4.2 Per-compartment
emissions for low data rate inside Wireless Avionics Intra-Communications
systems
A-4.3 Per-area
emissions for low data rate outside Wireless Avionics Intra-Communications
systems
A-4.4 Per-compartment
emissions for high data rate inside Wireless Avionics Intra-Communications
systems
A-4.5 Per-area
emissions for high data rate outside Wireless Avionics Intra-Communications
systems
Annex 5 List of acronyms