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AFDX 入门资料 AFDX/ARINC 664 Protocol Tutorial
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AFDX入门资料,GE的。 AFDX/ARINC 664 Protocol Tutorial。。。。。
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GE Fanuc
Embedded Systems
AFDX/ARINC 664
Protocol
Tutorial
Table of Contents
Chapter 1 Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
The Antecedents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
What is AFDX? . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
Other Avionics Buses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
ARINC 429 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
MIL-STD-1553 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
Ethernet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
ALOHA Net . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
The ALOHA Protocol . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Ethernet Local Area Networks (Broadcast Media) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
The Ethernet Protocol . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Ethernet Using Category 5 UTP Copper Twisted Pairs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Ethernet Frame Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Chapter 2 Ethernet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Full-duplex, Switched Ethernet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Doing Away with Contention . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Reducing Wire Runs and Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Chapter 3 End Systems and Avionics Subsystems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
End Systems and Avionics Subsystems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
Chapter 4 AFDX Communications Ports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
AFDX Communications Ports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
Chapter 5 Virtual Links: Packet Routing in AFDX. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
Virtual Links . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
Chapter 6 Message Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
Message Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
Chapter 7 Redundancy Management. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Redundancy Management. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Chapter 8 Virtual Link Isolation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
Virtual Link Isolation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
Choosing the BAG and Lmax for a Virtual Link. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Chapter 9 Virtual Link Scheduling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Virtual Link Scheduling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Chapter 10 Jitter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
Jitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
Chapter 11 AFDX Message Structures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
Introduction. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
Implicit Message Structures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
ARINC 429 Labels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Chapter 12 The AFDX Protocol Stack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
The AFDX Protocol Stack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
Transmission . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
Reception . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
Appendix A AFDX Frame Addressing and Header Structures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Ethernet Addressing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
IP Header Format and Addressing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
UDP Header Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
Appendix B Referenced Documents. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
Reference List. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
List of Figures
Figure 1. AFDX Network . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
Figure 2. ARINC 429 Communication Protocol . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5
Figure 3. MIL-STD-1553 Bus Communication Protocol . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
Figure 4. ALOHA Net . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Figure 5. Ethernet Local Area Networks (Broadcast Media). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Figure 6. Ethernet Frame Format . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Figure 7. Full-Duplex, Switched Ethernet Example . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Figure 8. AFDX versus ARINC 429 architecture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Figure 9. End Systems and Avionics Subsystems Example . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
Figure 10. Sampling Port at Receiver . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
Figure 11. Queuing Port at Receiver. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
Figure 12. Format of Ethernet Destination Address in AFDX Network . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
Figure 13. Packet Routing Example . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
Figure 14. Message Sent to Port 1 by the Avionics Subsystem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
Figure 15. Ethernet Frame with IP and UDP Headers and Payloads . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
Figure 16. A and B Networks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Figure 17. AFDX Frame and Sequence Number. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Figure 18. Receive Processing of Ethernet Frames. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Figure 19. Three Virtual Links Carried by a Physical Link . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
Figure 20. Virtual Link Scheduling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Figure 21. Virtual Link Scheduling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Figure 22. Role of Virtual Link Regulation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
Figure 23. Two Message Structures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
Figure 24. ARINC 664 Message Structures. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Figure 25. AFDX Tx Protocol Stack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
Figure 26. AFDX Rx Protocol Stack. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
Figure 27. Ethernet Source Address Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Figure 28. IP Header Format . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Figure 29. IP Unicast Address Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Figure 30. IP Multicast Address Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
Figure 31. UDP Header Format. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
4
One of the reasons that AFDX is such an attractive tech-
nology is that it is based upon Ethernet, a mature technol-
ogy that has been continually enhanced, ever since its
inception in 1972. In fact, the commercial investment and
advancements in Ethernet have been huge compared say,
to ARINC 429, MIL-STD-1553, and other specialized data-
communications technologies.
As shown in Figure 1, an AFDX system comprises the follow-
ing components:
Avionics Subsystem: The traditional Avionics Subsystems
on board an aircraft, such as the flight control com-
puter, global positioning system, tire pressure monitoring
system, etc. An Avionics Computer System provides a
computational environment for the Avionics Subsystems.
Each Avionics Computer System contains an embedded
End System that connects the Avionics Subsystems to an
AFDX Interconnect.
AFDX End System (End System): Provides an “interface”
between the Avionics Subsystems and the AFDX Intercon-
nect. Each Avionics Subsystem the End System interface
to guarantee a secure and reliable data interchange with
other Avionics Subsystems. This interface exports an ap-
plication program interface (API) to the various Avionics
Subsystems, enabling them to communicate with each
other through a simple message interface.
AFDX Interconnect: A full-duplex, switched Ethernet in-
terconnect. It generally consists of a network of switches
that forward Ethernet frames to their appropriate destina-
tions. This switched Ethernet technology is a departure
from the traditional ARINC 429 unidirectional, point-to-
point technology and the MIL-STD-1553 bus technology.
Chapter 1 Overview
The Antecedents
Moving information between avionics subsystems on board
an aircraft has never been more crucial, and it is here that
electronic data transfer is playing a greater role than ever
before. Since its entry into commercial airplane service on the
Airbus A320 in 1988, the all-electronic fly-by-wire system has
gained such popularity that it is becoming the only control
system used on new airliners.
But there are a host of other systems — inertial platforms,
communication systems, and the like — on aircraft, that
demand high-reliability, high-speed communications, as well.
Control systems and avionics in particular, rely on having
complete and up-to-date data delivered from source to re-
ceiver in a timely fashion. For safety-critical systems, reliable
real-time communications links are essential.
That is where AFDX comes in. Initiated by Airbus in the evolu-
tion of its A380 Aircraft, they coined the term, AFDX, for Avion-
ics Full-DupleX, switched Ethernet. AFDX brings a number of
improvements such as higher-speed data transfer — and with
regard to the host airframe — significantly less wiring, thereby
reducing wire runs and the attendant weight.
What is AFDX?
Avionics Full DupleX Switched Ethernet (AFDX) is a standard
that defines the electrical and protocol specifications (IEEE
802.3 and ARINC 664, Part 7) for the exchange of data be-
tween Avionics Subsystems. One thousand times faster than
its predecessor, ARINC 429, it builds upon the original AFDX
concepts introduced by Airbus.
Figure 1. AFDX Network
Controllers
Actuators
Sensors
Controllers
Actuators
Sensors
Gateway
Avionics Computer System
AFDX
Interconnect
End
System
Avionics
Subsystem
Avionics
Subsystem
End
System
End
System
Avionics Computer System
Avionics Computer System
Internet
5
As shown in the example in Figure 1, two of the End Systems
provide communication interfaces for three avionics sub-
systems and the third End System supplies an interface for a
Gateway application. It, in turn, provides a communications
path between the Avionics Subsystems and the external IP
network and, typically, is used for data loading and logging.
The following sections provide an overview of the AFDX ar-
chitecture and protocol. But first we briefly review two of the
traditional avionics communications protocols.
Other Avionics Buses
This section compares AFDX to two earlier Avionics data com-
munication protocols: ARINC 429 and MIL-STD-1553.
ARINC 429
Receiver ReceiverReceiverReceiver
Source
Bit rates are either 100 Kbps or 12.5 Kbps
32-bit messages
Figure 2. ARINC 429 Communication Protocol
ARINC 429 implements a single-source, multi-drop bus with
up to 20 receivers (see Figure 2). Messages consist of 32-bit
words with a format that includes five primary fields. The
Label field determines the interpretation of the fields in the re-
mainder of the word, including the method of translation. The
point to multi-point property of ARINC 429 requires the Avion-
ics system to include an ARINC 429 bus for each pair-wise
communication. Refer to the GE Fanuc Embedded Systems
ARINC Tutorial for more details.
MIL-STD-1553
Bit-rate 1 Mbps
20-bit data word
Figure 3. MIL-STD-1553 Bus Communication Protocol
MIL-STD-1553 (see Figure 3) implements a bus architecture
in which all the devices attached to the bus are capable of
receiving and transmitting data. The Avionics subsystems at-
tach to the bus through an interface called a remote terminal
(RT). The Tx and Rx activity of the bus is managed by a bus
controller, that acts to ensure that no two devices ever trans-
mit simultaneously on the bus. The communication is half
duplex and asynchronous. For more information, refer to the
GE Fanuc Embedded Systems “MIL-STD-1553 Tutorial”.
BC
RT
RT
RTRT
MIL-STD 1553 DATA BUS
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