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Guidelines for the use of GNSS in surveying and mapping

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7.4.4 System <strong>in</strong>itialisation<br />

Operational procedures are generally simple; with a<br />

dual-frequency receiver, <strong>in</strong>itialisation is fully<br />

automatic <strong>and</strong> can be realised while static or while<br />

mov<strong>in</strong>g (on-<strong>the</strong>-fly). Fully automatic <strong>in</strong>itialisation,<br />

under normal conditions, is usually achieved<br />

reliably with<strong>in</strong> a m<strong>in</strong>ute or so. To achieve centimetre<br />

accuracies, <strong>the</strong> rover tracks carrier phase <strong>and</strong> code<br />

phase (pseudorange) data <strong>and</strong> must <strong>in</strong>itialise itself<br />

with respect to <strong>the</strong> base station. Initialisation is <strong>the</strong><br />

term <strong>use</strong>d to def<strong>in</strong>e <strong>the</strong> process <strong>of</strong> determ<strong>in</strong><strong>in</strong>g <strong>the</strong><br />

carrier phase <strong>in</strong>teger ambiguities; at least five<br />

common satellites must be tracked between <strong>the</strong><br />

base station <strong>and</strong> rover with a PDOP <strong>of</strong> better than<br />

five. Be<strong>for</strong>e <strong>in</strong>itialisation, <strong>the</strong> receiver may produce<br />

a coarser solution, with<strong>in</strong> about a metre, but can<br />

converge with<strong>in</strong> a m<strong>in</strong>ute or so to a few<br />

centimetres. Once <strong>in</strong>itialised, <strong>the</strong> system switches<br />

to a fixed solution (ambiguities resolved) <strong>and</strong><br />

precision improves to about a centimetre.<br />

7.4.5 Incorrect <strong>in</strong>itialisations<br />

The <strong>in</strong>itialisation process is very reliable, but<br />

<strong>in</strong>correct <strong>in</strong>itialisations can occur. Formal test<strong>in</strong>g by<br />

a manufacturer should <strong>in</strong>dicate <strong>in</strong>itialisation<br />

reliability figures <strong>of</strong> at least 99.75 per cent. The<br />

level <strong>of</strong> reliability may also be a function <strong>of</strong> time,<br />

with less reliable <strong>in</strong>itialisation figures be<strong>in</strong>g specified<br />

<strong>for</strong> shorter <strong>in</strong>itialisation periods. Different systems<br />

respond <strong>in</strong> various ways, <strong>and</strong> this should be taken<br />

<strong>in</strong>to consideration when prepar<strong>in</strong>g quality<br />

procedures. In all cases, best practice is to <strong>in</strong>itialise<br />

<strong>in</strong> completely open areas with no possibility <strong>of</strong><br />

multipath or o<strong>the</strong>r <strong>in</strong>terference to satellite track<strong>in</strong>g.<br />

For RTK <strong>in</strong>itialisations, <strong>the</strong> production <strong>of</strong> three<br />

dist<strong>in</strong>ct quality control parameters is recommended:<br />

+ <strong>the</strong> ITRS89 co-ord<strong>in</strong>ates <strong>of</strong> each <strong>in</strong>itialisation<br />

po<strong>in</strong>t, <strong>the</strong>ir accuracy at <strong>the</strong> 95 per cent<br />

confidence level <strong>and</strong> <strong>the</strong> type <strong>of</strong> <strong>in</strong>itialisation<br />

(i.e. known po<strong>in</strong>t, on-<strong>the</strong>-fly, etc.)<br />

+ <strong>in</strong>teger bias values <strong>of</strong> <strong>the</strong> <strong>in</strong>itialisation basel<strong>in</strong>e<br />

solution<br />

+ ratio, variance, RMS <strong>of</strong> <strong>the</strong> <strong>in</strong>itialisation<br />

basel<strong>in</strong>e.<br />

These latter two items should be provided by <strong>the</strong><br />

s<strong>of</strong>tware to give <strong>the</strong> surveyor an <strong>in</strong>dication <strong>of</strong> <strong>the</strong><br />

reliability <strong>of</strong> each <strong>in</strong>itialisation, <strong>and</strong> should be<br />

checked after each re-<strong>in</strong>itialisation with a duplicate<br />

field po<strong>in</strong>t taken to provide a physical check. All<br />

three should be logged as explicit quality control<br />

parameters <strong>in</strong> <strong>the</strong> survey archive <strong>for</strong> each<br />

<strong>in</strong>itialisation <strong>and</strong> given <strong>in</strong> <strong>the</strong> f<strong>in</strong>al report if required.<br />

7.4.6 Initialisation checks<br />

A bad <strong>in</strong>itialisation may result <strong>in</strong> position errors <strong>of</strong><br />

at least 20 centimetres. The receiver may<br />

automatically detect <strong>and</strong> correct <strong>the</strong>se events,<br />

given suitable satellite availability <strong>and</strong> geometry.<br />

This would normally take a few m<strong>in</strong>utes, <strong>and</strong> this<br />

time could be considered as an <strong>in</strong>itialisation or selfcheck<strong>in</strong>g<br />

w<strong>in</strong>dow. The rare occurrences <strong>of</strong> bad<br />

<strong>in</strong>itialisations tend to be foc<strong>use</strong>d around lack <strong>of</strong><br />

redundant satellite coverage or poor PDOP (e.g.<br />

five satellites only with a marg<strong>in</strong>al PDOP), or at<br />

heavily multipa<strong>the</strong>d locations. Operational<br />

procedures, such as satellite coverage plann<strong>in</strong>g or<br />

check<strong>in</strong>g aga<strong>in</strong>st known po<strong>in</strong>ts, are best practice <strong>in</strong><br />

<strong>the</strong>se cases.<br />

Similarly, observation periods where an <strong>in</strong>itialisation<br />

has been followed quickly by a loss <strong>of</strong> lock <strong>and</strong><br />

re-<strong>in</strong>itialisation (i.e. with<strong>in</strong> <strong>the</strong> time <strong>of</strong> a selfcheck<strong>in</strong>g<br />

w<strong>in</strong>dow) should be treated as suspect,<br />

<strong>and</strong> two checks should be done at known po<strong>in</strong>ts <strong>in</strong><br />

this segment.<br />

A fixed solution, whilst requir<strong>in</strong>g five satellites to<br />

<strong>in</strong>itialise, can be ma<strong>in</strong>ta<strong>in</strong>ed through periods when<br />

only track<strong>in</strong>g four satellites. In addition <strong>the</strong> fixed<br />

solution can be ma<strong>in</strong>ta<strong>in</strong>ed through periods when<br />

<strong>the</strong> communications l<strong>in</strong>k is lost. The<br />

communications l<strong>in</strong>k provides satellite observations<br />

from <strong>the</strong> base station at <strong>the</strong> rover, <strong>in</strong> order that <strong>the</strong><br />

firmware can compute <strong>the</strong> <strong>in</strong>itialisation basel<strong>in</strong>e<br />

solution. It is best practice to note when <strong>the</strong><br />

communications l<strong>in</strong>k is lost, <strong>and</strong> to re-process any<br />

po<strong>in</strong>ts captured, us<strong>in</strong>g post-process<strong>in</strong>g s<strong>of</strong>tware. In<br />

most cases <strong>the</strong> RTK equipment will flag <strong>the</strong><br />

observations, but it is good practice to log <strong>the</strong>se<br />

po<strong>in</strong>ts on a suitable book<strong>in</strong>g sheet <strong>in</strong> <strong>the</strong> field. If<br />

satellite lock is also lost when <strong>the</strong> communications<br />

l<strong>in</strong>k is down, it is good practice to complete a<br />

period <strong>of</strong> static <strong>in</strong>itialisation accord<strong>in</strong>g to <strong>the</strong><br />

medium-precision static criteria given <strong>in</strong> section<br />

1.3.<br />

It is best practice, however, to ensure that <strong>the</strong><br />

communications l<strong>in</strong>k is ma<strong>in</strong>ta<strong>in</strong>ed <strong>for</strong> <strong>in</strong>itialisations<br />

<strong>and</strong> survey po<strong>in</strong>ts.<br />

This can be done by plann<strong>in</strong>g <strong>the</strong> survey to ensure<br />

RTK basel<strong>in</strong>es are kept short <strong>and</strong> <strong>the</strong> survey takes<br />

54 | GUIDELINES FOR THE USE OF <strong>GNSS</strong> IN LAND SURVEYING AND MAPPING

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