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Technical Details
The heart of the RWS system is the RWS Control Electronics Unit. This space computer
features 2 Central Processing Unit (CPU) cards, 2 - 1553 interface cards, 3 video
cards, 1 analog / digital card and an Electronic Power Conditioner. The CPU cards
are based on MDA's Radiation Hardened 80386 DX microprocessor and a 80387 co-processor.
All of the electronic cards are interconnected by an Industry Standard Architecture
(ISA) bus, with the exception of the video cards, which are connected, by a VESA
Local bus.
The software running in the control electronics unit comprises the Workstation Host
Software, the Video Graphics Software and the Operations Control Software.
The Workstation Host Software is the operating system and data bus interface.
The Video Graphics Software, also provided by MDA, controls the video displayed
to the astronaut on the three monitors. This VGS also provides system parameters
overlaid on the video picture. The Operations Control Software, developed
by MDA in Richmond, provides the control and coordination for
all of the MSS elements - the Space Station Remote Manipulator System, the Mobile
Base System and the Special Purpose Dexterous Manipulator.
The RWS flight units were designed to be mounted in a standard USL rack and installed
in the U.S. Lab Module on the Space Station. In anticipation of the eventual installation
in the Space Station cupola, one RWS unit will be moved into the Cupola. This will
enable the astronauts controlling the MSS to augment the video views provided by
the RWS with views of the Space Station through the Cupola windows.
The RWS was launched March 8th on STS-102 Station flight 5A.1.
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