http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-0704063-A1

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filingDate 1994-06-16-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a40cf91f5cf6c11613932cdd32ffe7fb
publicationDate 1996-04-03-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-0704063-A1
titleOfInvention Satellite positioning system filter
abstract A method and associated algorithm for filtering time-varying location solution coordinates Px,n, Py,n and Pz,n (301) determined by a Satellite Positioning System (SATPS), which operates in a static mode and a dynamic mode (303), to reduce large discontinuities and control the rate at which a changing sequence of measurement errors can induce a change in a sequence of position solutions. The method forms sequences of filtered location coordinates {P^x,n}, {P^y,n} and {P^z,n} (325), smoothed to reduce discontinuities that occur with a changing set of measurement errors. The filtered location coordinates P^x,n, P^y,n and P^z,n (325) are formed as linear combinations of the respective unfiltered location solutions Px,n, Py,n and Pz,n (301) with predicted location coordinates P^x,n-, P^y,n- and P^z,n-. The predicted location coordinates for the present fix time t=tn are formed by projecting ahead the respective preceding filtered location coordinates P^x,n-1, P^y,n-1 and P^z,n-1 for the preceding fix time t=tn-1, using the respective average velocities sqrt(Vx,n + Vx,n-1), sqrt(Vy,n + Vy,n-1) and sqrt(Vz,n + Vz,n-1) in the time interval tn-1 ≤ t ≥ tn.
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Total number of triples: 28.