Continuous tracking of GPS signals in dynamic scenarios pose a significant
challenge for the design of the tracking loops. Optimising a design
to suit a particular scenario may degrade its performance in other
scenarios. For instance, increasing the carrier tracking loop bandwidth
to receive dynamic signals will inadvertently affect the accuracy
of the raw measurements. Therefore, in a stand-alone GPS receiver,
a trade-off design is required to perform optimally in all the scenarios.
External sensor integration with the GPS is considered as an alternative
to improve upon this, and INS is the ideal choice as it is not only
autonomous but also provides attitude at higher data rates.
Traditionally, the integration of GPS and INS were carried out in
loosely and tightly-coupled configurations. While these systems offer
significant advantages over the stand-alone GPS, nevertheless, it
is imperative to improve the performance wherever possible. Ultra-tight
integration, also called "deep level tracking", integrates
the I (in-phase) and Q (quadrature) signals from the tracking loops
of the GPS receiver with the position and velocity obtained from the
INS. The primary advantage of this configuration, in addition to the
benefits of loosely and tightly-coupled systems, is a significant
reduction of the tracking loops bandwidth, as the Doppler signal derived
from INS aids the tracking loop to remove the dynamics from the GPS
signals. Two important advantages stem from the reduction of the bandwidth:
accuracy of the raw measurements, and increased immunity to jamming
signals. The block diagram representing the 3 architectures are shown
in Figure 1.

Figure 1: Block Diagram of Loose, Tight and Ultra-Tight Integration
System
Unlike the loosely and tightly-coupled systems, which are considered
to be 'feed forward', ultra-tight systems are 'feedback' systems,
i.e., a feedback signal in the form of Doppler derived from the INS
also drives the tracking loops. For the successful implementation
of this system, the accuracy of the Doppler signal is very critical.
The errors that degrade the Doppler accuracy are the residual biases
in the estimates of integration Kalman filter. It is well known that
inertial sensors suffer from systematic and stochastic biases, which
degrade the navigation solution. Though the systematic bias is effectively
removed by the integration Kalman filter through incorporation of
GPS measurements, nevertheless, the stochastic component needs a different
treatment. Appropriate modelling techniques, like Gauss Markov and
Autoregressive, effectively mitigate this noise.
Conventional tracking loops obtain their feedback from within the
channel. The Costas phase discriminator, which is the central part
of the carrier tracking loop, generates the corrections from I and
Q measurements. These corrections, after filtering, drive the NCO
(Numerically Controlled Oscillator), which generates the quadrature
signals to reduce the error with the incoming signals. This configuration
is suitable for a system with low dynamics. However, as dynamics increase,
the phase error transcends the threshold thereby loosing lock. Therefore,
in the case of ultra-tight receivers, the NCO gets its correction
signal not only from within the channel, but also from the INS. This
additional signal from the INS removes the dynamics from the GPS signal
and subsequently keeps the loop in lock. The feedback from the INS
is the key to the ultra-tight receiverÕs performance. Figure 2 shows
the ultra-tight tracking loop architecture.

Figure 2: Ultra-tight tracking loop architecture
Though the inertial aiding of the tracking loops seems to be attractive,
if the aiding signal does not properly represent the true Doppler,
it results in a tracking loop bias, which degrades the phase output
of the Costas discriminator. This phenomenon, which is unseen in stand-alone
systems, is prevalent in ultra-tight receivers or receivers with Doppler
aiding. Ultimately, the challenge lies in removing any of the undesired
effects created by the aiding signal.
Tracking Loop Performance. The tracking performance of the
ultra-tight loop is compared with a conventional loop. The conventional
loops have a limitation on the dynamics to be handled, and when the
dynamics exceed the bandwidth, they switch back to wideband PLL or
narrowband FLL (frequency lock loop) temporarily relinquishing the
measurements for the navigation algorithm. This situation is aggravated
in urban areas, indoors, etc. However, ultra-tight loops remain in
the narrowband PLL mode even during high dynamics. Figure 3 shows
a plot comparing the conventional and ultra-tight tracking loops for
a constant velocity trajectory. While the conventional loops increase
in frequency with the input, the ultra-tight loops with a bandwidth
of only 3Hz maintain almost a constant Doppler.

Figure 3: Ultra-tight (BW = 3Hz) and Conventional (BW = 13Hz)
tracking loops performance
The feedback Doppler signal removes most of the dynamics from GPS
signals rendering the signal to be ÔalmostÕ dynamic-free. So, any
residual dynamics on GPS signals to be tracked is only due to the
local oscillator. As the Doppler due to oscillator is much less, carrier
bandwidth can be reduced significantly improving the accuracy of raw
measurements and anti-jam performance of the receiver.
Some preliminary research results were presented in:
-
BABU, R., 2004. Mitigating the correlations
in INS-aided GPS tracking loop measurements: A Kalman filter
based approach.
17th Int. Tech. Meeting of the Satellite
Division of the U.S. Institute of Navigation, Long Beach,
California, 21-24 September, 1566-1574.
(Download PDF)
-
BABU, R., & WANG, J., 2004. Improving the quality
of IMU-derived Doppler estimates for ultra-tight GPS/INS integration.
GNSS2004, Rotterdam, The Netherlands, 16-19 May, CD-ROM
proc., paper 144.
(Download PDF)