11.3.5.2 PDOP
The attitude determination accuracy is influenced by the satellite geometry the same
way as position accuracy. Poor satellite geometry results in less accurate position and
attitude determination.
11.3.5.3 Antenna Location
Antenna location errors are a minimum when the two position difference vectors are
orthogonal. Simulation results indicate that acceptable performance can be obtained
when the vectors intersect at an angle between 45 degrees and 135 degrees. The
performance deteriorates rapidly outside this domain.
11.3.5.4 Antenna Position Difference Uncertainty in the Body Frame
Uncertainty of the difference vectors in body coordinates is a function of two primary
factors: body flexure and errors inherit ed from the calibration process. Body flexure
alters the relative position between antennas, hence causing errors.
11.3.5.5 Measurement Accuracy and Error Budget
The most significant factor influencing the feasibility of GPS attitude measurement is
the accuracy of the range difference measurement. The error sources affecting
accuracy are as follows:
1.
Atmospheric delays
2.
Multipath effects which can be quite significant, but can be largely negated
by proper antenna placement
3.
Phase difference measurement accuracy
4.
Transmission delay stability
Very little is published about what accuracies can be expected when using GPS for
attitude reference, but one manufacturer claims a heading accuracy of 0.3 degree, roll
and pitch accuracy of 1.0 degree, updated at a 20 Hz rate with no practical speed limit,
a maximum acceleration of 10 G, and a maximum angular velocity of 30 degrees/sec.
The same manufacturer claims a heading accuracy of 0.05 degrees within 5 minutes in
a stationary mode. This performance is with a C/A code receiver, using 3 antennas
placed in a triangle with 57 cm baseline between the antennas. Generally, the
measurement accuracy depends on baseline length and measurement time. Longer
baselines and longer measurement times will improve the accuracy.
11 6
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