Table A 3. Almanacs
Parameter
NAVSTAR
GLONASS
1
week of validity
day of validity
2
identifier
channel number
3
eccentricity
4
inclination
5
time of almanac
equator crossing time
6
health
validity of almanac
7
right ascension ascending node (RAAN)
equator crossing longitude
8
rate of change of RAAN
9
root of semi major axis
orbital period
10
argument of perigee
argument of perigee
11
mean anomaly
12
luni solar term
13
time offset
time offset
14
frequency offset
equivalent. The primary purpose of almanac data is to allow the user to predict in
approximate terms the visible satellites and their geometry.
Almanac data provides a position of each satellite to within 100 200 m similar to GPS
almanacs. However, the inclusion in the GLONASS almanac of a luni solar correction
term implies a position error perhaps an order of magnitude better than a Navstar
almanac over an extended time period. The luni solar term remains substantially
constant for satellites with the same Right Ascension. Although the almanac is valid for
several days they are usually but not always changed every day in GLONASS at local
midnight.
It is interesting to observe that the GLONASS almanacs differ from the earlier Cicada
almanacs in one major respect. The earlier almanacs were based on an equitial tial
Kepler set where eccentricity and argument of the perigee are transmitted as h = e x
sinw and 1 = e x cosw. The equinoctial set of elements is suitable for orbits with small
eccentricity since it leads to equations with no singularities when e tends to zero.
A.14 NAVIGATION REFERENCE FRAME
GLONASS employs a geocentric cartesian system designated SGS85. The difference
from the GPS WGS84 frame is not large. Misra, Ref 8 reported differences of less than
20 m RMS. The two coordinate frames may be brought together by a small rotation
0.6" (3.10
6
rad) of the z axis and a 4 m displacement of the origin along the z axis.
Recently there has been a suggestion that the GLONASS coordinate frame has been
updated to a SGS90 designation.
A 14
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