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Advanced Avionics
By John C. Colwell, Bishop &
Associates Inc.
The gestation period
for highly complex systems, such as military and commercial aircraft,
can take as much as a decade, or five generations of Moore’s Law. As a
result, the initial conceptualization of systems and performance
requirements become moving targets. In the case of the F-22 Raptor, the
Intel processors initially selected for the common integrated processor
(CIP) were already out of production by the time the aircraft itself
entered production. Clearly, a new approach was needed.
In the traditional acquisition model, the system context—or
conceptualization—was defined first, and then driven primarily by the
mission requirements. The architecture and design phase would follow,
and finally, the program would move into the implementation phase. The
new model involves the dynamic interaction, from program start to
finish, between the system context, the system architecture and design,
and the commercial items available in the marketplace.

Traditional vs. COTS System Acquisition Model
The key advantage of
this approach is that the avionics system designer can leverage the
latest technology and performance advantages that are independently
driven by the commercial industry sectors, in particular,
telecommunications and computers. The elegant evolution of VME backplane
standards and Ethernet represent classic examples of this process.
From an electronic packaging and interconnection viewpoint, commercial
off-the-shelf procurement (COTS) takes us to a standards-based imbedded
systems approach to system architecture for avionics, mission computing,
and similar applications. The VPX (VITA 46), and more specifically, its
hardened version (VITA 48) standard is the platform of choice for the
F-22 Raptor, because of its ruggedness, ability to handle a diverse
array of system challenges, and its extensive I/O handling capabilities.
Also known as VPX-REDI (ruggedized enhanced design implementation), VITA
48 has three versions: V48.1 air-cooled, V48.2 conduction-cooled, and
V48.3 liquid-cooled. In its current implementation, the F-22 utilizes
the liquid flow through (LFT) method of cooling. A pair of liquid
distribution rails provides
polyalphaolefin (PAO),
or similar coolant, to the modules by means of quick disconnects, or QDs.
The backplane interconnect system for VPX (VITA 46) and VPX-REDI (VITA
48) is the multi-gig MT 2 product developed and manufactured by Tyco
Electronics Inc.
There are three versions of VPX-REDI modules based on the method of
cooling. There are two module sizes: 3U and 6U by 160mm. There are also
mezzanine boards.
The LFT cooling system also requires a method of interconnection between
the backplane distribution rail and the module. The coolant interconnect
is referred to as a quick disconnect, and is illustrated at the right.


The backplane
interconnect system was chosen by VITA because of its high bandwidth
capability, ESD and grounding characteristics, signal density, and
ruggedness. These attributes are essential to military avionics systems
due to the rapidly increasing number of very high-speed on-board
sensors, as well as the growing level of communications with ground,
in-flight, and space-based resources.

While the switching
fabrics, processors, and backplanes are COTS, the I/O and cable
assemblies are typically not. The interconnect cabling between the
backplane and the enclosure I/O is generally custom designed for the
intended application environment. Flexible circuit assemblies are
commonly employed in this application. The same applies to external
cable assemblies that link the computer to sensors and other black
boxes.
And in spite of the fact that the communication protocol may be
Avionics Full DupleX
Switched Ethernet (AFDX), introduced by Airbus in its A380 commercial
craft, or Fibre Channel, which is being deployed in the F-35 Joint
Strike Fighter (JSF), the I/O interconnects remain mil-spec
circular in nature. The F-22 utilizes a mix of Category 5
shielded twisted-pair and fiber optic cables, whereas the F-35 utilizes
a predominantly fiber optic network. Both aircraft will continue to
support legacy systems and sensors using the older
MIL-STD-1553 copper bus
networks.
Harris Corp. Government Communications Systems Division in Melbourne,
Florida, holds the contract for the F-35’s advanced avionics design from
Northrop Grumman. The contract includes fiber optic transceivers and
physical hardware to provide four channels of data transmission and
reception at a data rate of two gigabits per second over the aircraft's
extensive fiber optic network. Other significant avionics contractors
include Boeing, Mercury Computer Systems, Curtiss-Wright, and GE Fanuc
Embedded Systems.
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John Colwell
Director, Telecom, Medical and Instrumentation, Bishop &
Associates Inc.
John
Colwell’s background includes 10 years at Nortel
Networks‑Cable Group, where he directed the U.S. premises
cable marketing effort. In addition, Colwell directed
Nortel's global product development group. Prior to joining
Nortel, Colwell held positions in engineering, business
planning and development at Amphenol Corporation.
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