
Chapter 1 SPAN CPT7 Overview
SPAN CPT7 Installation and Operation User Manual v3A 20
SPAN CPT7 technical specifications are provided in SPAN CPT7 Technical Specifications on
page144.
1.1 Fundamentals of GNSS+INS
GNSS positioning observes range measurements from orbiting GNSS satellites. From these
observations, the receiver can compute position and velocity with high accuracy. NovAtel GNSS
positioning systems are highly accurate positioning tools. However, GNSS in general has some
restrictions which limit its usefulness in some situations. GNSS positioning requires line of sight
view to at least four satellites simultaneously. If these criteria are met, differential GNSS pos-
itioning can be accurate to within a few centimetres. If however, some or all of the satellite sig-
nals are blocked, the accuracy of the position reported by GNSS degrades substantially, or may
not be available at all.
In general, an INS uses forces and rotations measured by an IMU to calculate position, velocity
and attitude. This capability is embedded in the firmware of OEM7 receivers. Forces are meas-
ured by accelerometers in three perpendicular axes within the IMU and the gyros measure angu-
lar rotation rates around those axes. Over short periods of time, inertial navigation gives very
accurate acceleration, velocity and attitude output. The INS must have prior knowledge of its ini-
tial position, initial velocity, initial attitude, Earth rotation rate and gravity field. Since the IMU
measures changes in orientation and acceleration, the INS determines changes in position and
attitude, but initial values for these parameters must be provided from an external source. Once
these parameters are known, an INS is capable of providing an autonomous solution with no
external inputs. However, because of errors in the IMU measurements that accumulate over
time, an inertial-only solution degrades with time unless external updates such as position, velo-
city or attitude are supplied.
The SPAN system’s combined GNSS+INS solution integrates the raw inertial measurements
with all available GNSS information to provide the optimum solution possible in any situation. By
using the high accuracy GNSS solution, the IMU errors can be modeled and mitigated. Con-
versely, the continuity and relative accuracy of the INS solution enables faster GNSS signal reac-
quisition and RTK solution convergence.
The advantages of using SPAN technology are its ability to:
lProvide a full attitude solution (roll, pitch and azimuth)
lProvide continuous solution output (in situations when a GNSS-only solution is impossible)
lProvide faster signal reacquisition and RTK solution resolution (over stand-alone GNSS
because of the tightly integrated GNSS and INS filters)
lOutput high-rate (up to the IMU data rate depending on your logging selections) position,
velocity and attitude solutions for high-dynamic applications, see also Logging Restriction
Important Notice on page84
lUse raw phase observation data (to constrain INS solution drift even when too few satellites
are available for a full GNSS solution)
For more information about GNSS and INS, refer to www.novatel.com/an-introduction-
to-gnss/