Military Embedded Systems - Fall 2005 - Volume 1 Number 2
Military Embedded Systems - Fall 2005 - Volume 1 Number 2
Military Embedded Systems - Fall 2005 - Volume 1 Number 2
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Industry Analysis<br />
Better architectures hit<br />
the ground<br />
One hears a great deal about transforming<br />
the military from the current platformcentric<br />
approach to network-centric operations.<br />
The underlying computer technologies,<br />
including chips and software, are<br />
also undergoing fundamental change, and<br />
it is good news for designers and users of<br />
military computers.<br />
Command Center aboard a heavily modified<br />
Boeing 707 aircraft known as the<br />
TACAMO, the system maintains communication<br />
and control in the event that<br />
other command centers are damaged<br />
or destroyed. It provides networking<br />
and routing within the aircraft, handling<br />
packetized radio, satellite, radar, and<br />
laser transmissions, and ties together<br />
different systems on the plane (see<br />
Figure 3, photo courtesy of Performance<br />
Technologies, Inc.).<br />
Performance Technologies has also<br />
developed a unique hybrid CompactPCI/<br />
Figure 2<br />
VME system for use in the Global Hawk<br />
UAV (see Figure 4, photo courtesy of<br />
Performance Technologies, Inc.). This<br />
computer provides near real-time highresolution<br />
images and intelligence to<br />
field commanders in theater or across<br />
the world. Multicast image streams can<br />
be ordered by a commander in a control<br />
room or a soldier on the ground in the<br />
next valley, providing vital current information<br />
and situational awareness. The<br />
CompactPCI boards are conduction cooled<br />
and compliant with the ANSI/VITA 30.1<br />
specification (2 mm connector practice for<br />
conduction-cooled Eurocard systems).<br />
Most backplane interconnect technologies,<br />
including VME and CompactPCI, are<br />
based on chip-level interconnects that<br />
were intended for planar motherboards.<br />
Hot swap was not an integral part of these<br />
interconnects, and their parallel nature<br />
has meant that any board plugged into the<br />
backplane could cause the entire system<br />
to fail if it failed. Full 2N redundancy was<br />
often the only solution. Focus was placed<br />
on reliability instead of the much more useful<br />
concept of availability because parallel<br />
bus architectures just do not adapt well<br />
to high availability designs, which require<br />
system management and failure domains<br />
of a single board. Also, as core chip<br />
voltages go ever lower, the notion of<br />
distributing chip supply voltages often<br />
means that parallel backplanes are required<br />
to produce hundreds, or even thousands,<br />
of amps of current for large systems.<br />
IP/Radio<br />
Ground Communications<br />
Satellite Uplink/Downlink<br />
Radars<br />
10/100/1000 TX<br />
RS-232/RS422/1553<br />
Connections<br />
Five<br />
<strong>Systems</strong>/Aircraft<br />
Command and Control<br />
Figure 3<br />
<strong>Military</strong> EMBEDDED SYSTEMS October <strong>2005</strong> / 13