uses measurements from a reference receiver established at a known location,
along with differencing algorithms, to remove common satellite and signal propaga  
tion errors from the PVT solutions of other (mobile) receivers operating in the
vicinity of the reference station. The residual errors that remain uncorrected are
due to multipath and noise in the receivers. DGPS techniques can be applied to the
real time PVT solution or to recorded measurement data.  Real time DGPS requires
a data link  pass the reference measurements to the mobile receiver(s). DGPS
techniques can be applied to nondifferential receivers if the raw measurement data
and navigation message are accessible.  There are two primary variations of the
differential techniques, one based on ranging code measurements and the other
based on carrier phase measurements.
Ranging code DGPS (RCD) techniques can be applied to receivers with any of the
tracking architectures described in the previous paragraphs.  For RCD,
measurements from the reference receiver are used at the receiver site to calculate
corrections, which are then broadcast to the mobile receivers.  The mobile
receivers incorporate the corrections into their PVT solution, thereby removing the
common errors and improving accuracy.
The reference receiver can develop corrections for the position solution or
individual satellite ranging signals.  If the corrections are provided for the position
solution, the correction is simply the difference between the measured PVT solution
and the "true" solution consisting of the surveyed location, zero velocity, and
precise or smoothed time. However in this case, the reference and user receivers
must either use the same satellites to calculate the same solution, or PVT
corrections for each possible combination of satellites must be broadcast.  It is
usually more efficient and flexible to broadcast corrections based on individual
satellite ranging errors, thereby allowing the user receiver to select the corrections
that are applicable to the particular set of satellites that it is tracking.  Real time
RCD is capable of producing accuracies on the order of 1 metre.
Carrier phase DGPS (CPD) systems essentially calculate the difference between
the reference location and the user location using the difference between the
carrier phases measured at the reference receiver and the user receiver.  In real 
time systems, carrier phase data from the reference receiver is broadcast to the
mobile receivers.  The mobile receivers use double differencing techniques to
remove the satellite and receiver clock biases, then use the phase differences to
determine the position of the mobile receiver with respect to the reference receiver
location.
Determining the initial phase offset (cycles plus fractional phase) between the
reference station and the mobile receiver has traditionally been a process that
required several minutes.   Therefore, it is important to maintain phase lock on the
carrier signals to maintain a continuous flow of position data and avoid
reinitialization.  Consequently, CPD systems have  traditionally used continuous
tracking receivers.  Receivers which gather measurements from more than four
satellites are common since they add robustness in the event of loss of lock on one
satellite and since additional satellites can reduce initialization time.  The CPD
techniques were originally developed for surveying applications where real time
data was not essential.  However, near real time and real ti me techniques are
under development with the goal of supporting applications such as precision 
approach for
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