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The GNSS integer ambiguities: estimation and validation

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Integer ambiguity resolution 3<br />

<strong>The</strong> problem of <strong>integer</strong> ambiguity resolution has drawn a lot of attention in the past<br />

decades. Many ambiguity resolution algorithms have been published. Not all of these<br />

algorithms will be discussed here; only a brief overview will be given. <strong>The</strong> first step<br />

of ambiguity resolution is <strong>integer</strong> <strong>estimation</strong>. <strong>The</strong>refore, section 3.1 starts with the<br />

definition of admissible <strong>integer</strong> estimators. For the quality description <strong>and</strong> <strong>validation</strong> of<br />

the estimators, their distribution functions are required. <strong>The</strong> distributional properties of<br />

the float <strong>and</strong> fixed ambiguity will be given in section 3.2, where it is also shown how the<br />

probability of correct <strong>integer</strong> <strong>estimation</strong>, the success rate, can be approximated. For the<br />

purpose of <strong>validation</strong>, the parameter distribution of the ambiguity residuals is required.<br />

This distribution function <strong>and</strong> its properties will be given in section 3.3. In section 3.4<br />

it is shown how the quality of the fixed baseline estimator can be expressed. Section 3.5<br />

gives an overview of currently available methods for the <strong>validation</strong> of the fixed ambiguity<br />

solution <strong>and</strong> their shortcomings. Finally, in section 3.6 a completely different approach<br />

of ambiguity resolution is described, namely the Bayesian approach.<br />

3.1 Integer <strong>estimation</strong><br />

Any <strong>GNSS</strong> observation model can be parameterized in <strong>integer</strong>s <strong>and</strong> non-<strong>integer</strong>s. This<br />

gives the following system of linear(ized) observation equations:<br />

y = A a + B b + e<br />

m×nn×1 m×pp×1 m×1<br />

m×1<br />

(3.1)<br />

where y is the GPS observation vector of order m, a <strong>and</strong> b are the unknown parameter<br />

vectors of dimension n <strong>and</strong> p respectively, <strong>and</strong> e is the noise vector. <strong>The</strong> data vector<br />

y usually consists of the observed-minus-computed DD phase <strong>and</strong>/or code observations<br />

on one, two or three frequencies <strong>and</strong> accumulated over all observation epochs. <strong>The</strong><br />

entries of the parameter vector a will then consist of the unknown <strong>integer</strong> carrier phase<br />

<strong>ambiguities</strong>, which are expressed in units of cycles rather than in units of range. It is<br />

known that the entries are <strong>integer</strong>s, so that a ∈ Z n . <strong>The</strong> remaining unknown parameters<br />

form the entries of the vector b. <strong>The</strong>se parameters may be the unknown baseline<br />

increments <strong>and</strong> for instance atmospheric (ionospheric, tropospheric) delays, which are<br />

all real-valued, i.e. b ∈ R p . <strong>The</strong>se real-valued parameters are referred to as the baseline<br />

parameters, although the vector b may thus contain other parameters than only the<br />

baseline components.<br />

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