SAC-C orbit reconstruction using the experimental GPS/GLONASS receiver LAGRANGE
2002
The Argentinian satellite SAC-C was launched in
November 2000. It carries onboard an experimental
prototype of the first Italian-built, combined
GPS/GLONASS space receiver LAGRANGE, developed
for the Italian Space Agency (ASI) by LABEN S.p.a. It
also carries a second GPS receiver provided by JPL known
as Blackjack. The SAC-C prototype of the LAGRANGE
receiver is based on the first-version of the Advanced
GPS/GLONASS ASIC (AGGA) developed by the
European Space Agency (ESA). The dual-frequency
LAGRANGE receiver is provided with 12 channels that
can be dynamically allocated to GPS and GLONASS
frequencies. The receiver was operating during a period of
56 days until 23 January 2001, when it suffered a
radiation-induced failure and ceased operations before the
end of the commissioning phase. However, data were
collected during the entire period and were made available
for analysis. This paper will address the results from the
LAGRANGE data processing. It is of interest to evaluate
the performance of this receiver based on the availability
of the well-known, long-heritage BlackJack receiver
onboard the same spacecraft. The two receiver antennas
were placed very to each other, thus allowing a very
similar satellite tracking scenario. In this experimental
setup the LAGRANGE receiver suffered from important
limitations such as channel-dependent pseudorange biases,
very low availability of measurements at the L2 frequency
and a clock with a very high drift.
A new strategy to cope with the biased pseudorange
measurements (“realignment”) was implemented, which
allowed to obtain a navigation solution otherwise
impossible. This strategy, based on the availability of
another GPS receiver (BlackJack), did not allow the
recovery of the absolute LAGRANGE clock error. This
important quantity was inferred through reference to a
precise orbit of the SAC-C satellite obtained using
BlackJack carrier phase data. An along-track orbit
difference was the key to calibrate the LAGRANGE clock.
The two receivers were later compared in their
performance in terms of an L1-only, doubly differenced
carrier phase-based Precise Orbit Determination analysis.
When the orbits obtained from single frequency data from
each of the two receivers are compared in an RTN
reference frame with the same precise reference orbit—
obtained from dual-frequency BlackJack data—the
residuals show very similar behavior in terms of both
mean and standard deviation. This can be interpreted as an
indication that the two receivers performances are quite
similar. Studies are ongoing to assess wether use of
combined iono-free pseudoranges and carrier phase
LAGRANGE measurements provide indications of a
better performance of the receiver when the comparisons
are made with the precise SAC-C orbit.
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