[MOIMS-NAV-EXEC] Data messages for re-entry and fragmentation events
Tim.Flohrer at esa.int
Tim.Flohrer at esa.int
Mon Sep 7 12:06:53 UTC 2015
Dear colleagues,
as mentioned and very briefly discussed at the last telecon of the MOIMS
Navigation Working Group, we are working at ESA on data formats that cover
the exchange of information on re-entry and fragmentation events. This
work has been triggered by actual needs from the operational support that
ESA's Space Debris Office is providing to missions, and, in parallel,
during the developments and architectural analysis performed in ESA's SSA
program in the Space Surveillance and Tracking (SST) segment. My colleague
Luis Martin (my predecessor in the working group for the SSA/SST) made a
first statement on planned developments at the London meeting of the
CCSDS.
With this email we want to provide to you additional information on both
formats. It would be very interesting for us to learn about your opinions
and expectations on whether such topics are of interest for a wider
community and, hence, on whether the working group may want to address
these needs.
We are ready to give more detailed presentations on the drafted data
messages at the Darmstadt meeting.
Best regards,
Tim and Alexandru
Re-entry Data Message (RDM)
The exchange of spacecraft re-entry event data has been developed for the
ESA SSA/SST project. The used format is inspired by CCSDS messages.
Satellite operators exchange several types of messages already covered by
CCSDS, describing orbits, observations, attitude state and conjunctions.
However, currently no message for spacecraft (re-)entry exists.
Predictions on re-entry epochs, sometimes also including the estimated
location, are already exchanged at technical level, e.g., in the frame of
test campaigns run by the Inter-Agency Space Debris Coordination Committee
(IADC). These test campaigns aim at comparing prediction techniques and
tools, and verifying readiness and technical expertise for high-risk
re-entry events. With an increase in Space Surveillance and Tracking (SST)
activities, it is expected that re-entry tracking campaigns will become
more frequent and the need for simpler, standardised data exchange will
increase. The developed format facilitates data sharing and
interoperability, for example for analysis and visualisation. For
instance, during the last orbits of a re-entering spacecraft, agency A
might not have the sensors to track the spacecraft, but agency B does and
provides up to date information about the re-entry (such as the projected
impact location), without having to exchange tracking data.
The Re-entry Data Message contains information about an object entering
the Earth's atmosphere. It is not intended to describe a controlled
re-entry, or a landing, or to provide detailed orbit information for the
object. Re-entry data are expected to be exchanged between entities
monitoring the space environment, spacecraft operators and national or
international authorities. The types of information currently exchanged in
re-entry monitoring campaigns include: object name, class and properties
(mass, cross-sectional area), the predicted epoch and location of the
re-entry event, and the concise description of used models.
A CCSDS-like Re-entry Data Message has been drafted for the ESA SSA/SST
system and aims at enabling a simpler exchange of re-entry data between
different entities and/or agencies.
Fragmentation Data Message (FDM)
The exchange of spacecraft fragmentation event descriptions has been
developed for the ESA SSA/SST project. The used format is inspired by
CCSDS messages.
A system observing the space environment and determining the orbits of the
covered objects can determine when and where a fragmentation event
occurred, and can issue the appropriate warnings. With an increase in
Space Surveillance and Tracking (SST) activities, it is expected that
fragmentation detection campaigns will become more frequent and the need
for simple, standardised data exchange will increase. The developed format
facilitates data sharing and interoperability, e.g., for analysis and
visualisation. For example, agency A does not have fragmentation detection
capabilities and a fragmentation event occurs in the same orbital regime
as one of its spacecraft. Agency B does have the capability and provides
agency A with the fragmentation information, which enables agency A to
assess the risk to its spacecraft, without having to exchange tracking
data.
The Fragmentation Data Message contains information about fragmentation
events in orbit around Earth. It is not intended to provide detailed orbit
information for the originator or the generated fragments. Fragmentation
data includes, as far as available, information about the progenitor
object (physical properties, COSPAR ID, etc.), spatial coordinates and
epoch of the fragmentation event, the spread in orbital properties of the
fragments, a list of fragments and their detection epochs, and the
increase in object spatial density due to the fragmentation event. If the
fragmentation was caused by a collision, the properties of the second
colliding spacecraft and the reference to the CDM describing the
conjunction can also be exchanged as an option.
A CCSDS-like Fragmentation Data Message has been drafted for the ESA
SSA/SST system and aims at enabling for a simpler exchange of
fragmentation data between different entities and/or agencies.
--
Tim Flohrer, PhD
ESA/ESOC Space Debris Office (HSO-GR)
Robert-Bosch-Strasse 5, DE-64293 Darmstadt, Germany
+49-6151-90-3058 (phone), +49-6151-90-2625 (fax)
http://www.esa.int/debris
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