Navman 11 User Manual

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MN002000A © 2004 Navman NZ Ltd. All rights reserved. Proprietary information and specifications subject to change without notice.
used to identify previously healthy satellites and 
to generate “working” visible satellite lists, while 
frequency standard data minimises satellite 
acquisition uncertainties. 
4.4.4 Frozen start
This state is entered if there are no valid data 
sources available (SRAM, RTC, EEPROM). This 
is considered to be a recovery mode because 
EEPROM should always contain valid information. 
An “out-of-the-box” board or a unit that has not 
operated for a significant amount of time (months) 
may approximate this state because the data in 
EEPROM may be valid but expired or partially 
complete.
4.5 Satellite management
This section describes the satellite management 
functions of the Jupiter family of GPS receivers.
4.5.1 Visible list generation.
A list of satellites visible to the receiver antenna 
is maintained whenever possible. A satellite is 
considered visible if its elevation in the sky is 
known to be above the horizon, if its almanac and 
ephemeris data indicate it is healthy, and if it has 
not been excluded by manual candidate satellite 
specification. Note that although a satellite is 
visible, its measurement is only available for use if 
the satellite is above the elevation mask angle.
The receiver’s channel resources are directed 
toward acquiring only those satellites which appear 
in this list except when the receiver is in cold start 
mode. Satellites within the list are ordered from 
highest to lowest elevation which, for sequential 
acquisition, also dictates the order in which 
acquisition attempts are made. 
Receiver position and current time are required 
to compute satellite positions from orbital data. 
If position and/ or time is not considered to be 
well known (i.e. their expected errors are large), 
then the list is extended below the horizon 
and is filled to the maximum of 12 satellites. If 
DGPS corrections are available, the satellites 
represented in the corrections are used to set the 
list membership instead, since they also represent 
satellites visible to a nearby transmitting DGPS 
base station. 
New visible satellite lists are generated by 
events that could cause a change in satellite list 
membership or could indicate a significant change 
in a satellite position relative to the antenna. These 
events include receipt of an elevation mask angle 
or candidate satellite specification command, 
downloading of a new satellite almanac, and 
changes in satellite health status reflected in new 
almanac or ephemeris data. 
In the case where DGPS corrections are used to 
establish list membership, a change in the set of 
satellites reflected in the corrections also causes a 
new list to be generated. During initial acquisition, 
a new list is generated when the receiver makes 
step adjustments to position and time. In the 
absence of these events, the visible satellite list is 
updated every 30 seconds. The visible satellite list 
is output in the Visible Satellites message (binary 
Message 1003)
4.5.1.1 Dilution Of Precision (DOP)
Geometric Dilution of Precision (GDOP) is a 
measure of the quality of a satellite constellation 
geometry. GDOP reflects the influence of satellite 
geometry on the accuracy of user position and 
time estimates. The best geometry is that which 
produces the lowest GDOP value. GDOP acts as a 
multiplier of the error in position and time estimates 
due to other sources. 
GDOP is a composite measure. It can be 
separated into:
• Position Dilution of Precision (PDOP)
PDOP reflects the effects of geometry on 
three-dimensional position estimates
• Time Dilution of Precision (TDOP)
TDOP reflects geometric effects on time 
estimates. The relationship can be expressed 
as:
GDOP =
In turn, PDOP can be separated into horizontal 
and vertical components: 
• Horizontal Dilution of Precision (HDOP) 
• Vertical Dilution of Precision (VDOP)
These components represent the effects of 
satellite geometry on two-dimensional horizontal 
position and on vertical position (altitude) 
estimates, respectively. 
This relationship can be expressed as:
PDOP =
The receiver computes the best available 
GDOP and each of its components in the Visible 
Satellites message (binary Message 1003). The 
best available GDOP is that associated with 
the satellite constellation consisting of all visible 
satellites above the mask angle (satellites whose 
measurements may be used). 
At least four satellites are required to estimate 
position and time, and therefore to compute a 
(PDOP)
2
 + (TDOP)
2
(HDOP)
2
 + (VDOP)
2