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Ground Systems
The TIMED Ground System has all
the facilities usually associated with space missions, such as operations
centers and ground stations. But TIMED was engineered as a total space-ground
system to streamline mission activities, so this Ground System is best understood
as a set of components that are tightly integrated with their counterparts
on the spacecraft. Figure 1 illustrates just how close this integration is.
The spacecraft components are shown on the left, and the ground components
on the right, but the physical distance and communications complexity that
separates them evaporates when one focuses on the strongly-coupled flows of
control and data
Figure 1. End-to-End
Data Flow in the TIMED System -- Click for enlarged view. Focusing on
the outside (green) loop in Figure 1, we can see on the right an investigator
in a Payload Operations Center (POC) who is generating a command to operate
his instrument. He sends this command on its way over the Internet in a packet
addressed to his instrument. The packet stops off briefly at a computer in
the Mission Operations Center (MOC) at APL. If the command is authentic and
there is a current radio link with the spacecraft, it is immediately transmitted
to the spacecraft's Command and Data Handling (C&DH) system. The
C&DH system automatically routes the command to the instrument, where
it is executed. The Instrument puts its collected science data into telemetry
packets that are addressed to the Mission Data Center (MDC) at APL. When a
downlink is available, the telemetry is transmitted to the MDC. Now, an investigator
at the POC (or anywhere else) can receive his (or anyone's) packets over
the Internet. He has two ways to receive his data: as packaged files or a
continuous time-ordered stream. He can see the packets as soon as they arrive
on the ground, but since all telemetry is archived and on-line in the MDC,
he may wait as long as he likes and then ask for a historical data stream. Notice that
there is also an inside (red) loop, almost entirely decoupled from the instruments,
that is dedicated to maintenance and operation of the spacecraft "bus",
which really includes everything needed to provide a comfortable "ride" to the four instruments on board. In this loop, we see a mission specialist
in the MOC who is generating command packets for the bus, perhaps to perform
a diagnostic test. The status of the bus is conveyed back to the MOC for assessment. To summarize
the essential feature of this architecture, the bus and instrument data loops
share common uplink and downlink services, but these services keep the operations
almost completely independent. eliminating the need for coordination between
bus and instrument operators for routine activities. This decoupling provides
substantial savings and simplification in the on-orbit mission operations. Now turning
to Figure 2, we see a more conventional view of the Ground System facilities
and their interconnections. The space-ground link is provided through a primary
ground station at APL, or via one of a network of offsite backup ground stations.
The equivalent path for pre-launch testing is through a special assembly of
Ground Support Equipment (GSE), also shown on the diagram. The red and blue
color-coded flows are the command and telemetry that support mission operations
already described.

Figure 2. TIMED
Ground System Architecture -- Click for enlarged view. Outlined in
Figure 2 is a special subdivision of the Ground System called the Science
Data System (SDS), which encompasses all science data analysis activities
in the TIMED program. We see here that each of the four instrument POCs is
actually subdivided into two areas, one for mission operations (MO), and the
other for data analysis (DA). The green and violet flows illustrate interchange
of science data among the many facilities involved, again over the Internet.
Although the science product archives are distributed among these facilities,
the MDC is a one-stop shop on the Web for locating and retrieving any of the
information gathered by the program.
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