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  • The paper presents a nonlinear analysis of position estimation based on a global navigation satellite system. A classical problem formulation and iterative solution that results in the weighted least squares estimate of the receiver state are assumed. The analysis employs the Taylor's theorem to express the nonlinear measurement model using the second order Taylor polynomial at the state estimate and the Lagrange form of the remainder. A sensitivity analysis of the Jacobian matrix pseudoinverse is performed, and an upper bound on the size of the quadratic term is derived using eigenstructure of the Hessian matrix. The results obtained show that both the sensitivity of the pseudoinverse and the size of the quadratic term are not significant, and thus the linear approximation commonly used to derive stochastic properties of the state estimate is reasonable. Although this result has been experimentally confirmed by numerous successful applications, this analysis can serve as a more rigorous basis when the design procedures for safety critical system have to be satisfied.
  • The paper presents a nonlinear analysis of position estimation based on a global navigation satellite system. A classical problem formulation and iterative solution that results in the weighted least squares estimate of the receiver state are assumed. The analysis employs the Taylor's theorem to express the nonlinear measurement model using the second order Taylor polynomial at the state estimate and the Lagrange form of the remainder. A sensitivity analysis of the Jacobian matrix pseudoinverse is performed, and an upper bound on the size of the quadratic term is derived using eigenstructure of the Hessian matrix. The results obtained show that both the sensitivity of the pseudoinverse and the size of the quadratic term are not significant, and thus the linear approximation commonly used to derive stochastic properties of the state estimate is reasonable. Although this result has been experimentally confirmed by numerous successful applications, this analysis can serve as a more rigorous basis when the design procedures for safety critical system have to be satisfied. (en)
Title
  • Nonlinear analysis of position estimate in global navigation satellite systems
  • Nonlinear analysis of position estimate in global navigation satellite systems (en)
skos:prefLabel
  • Nonlinear analysis of position estimate in global navigation satellite systems
  • Nonlinear analysis of position estimate in global navigation satellite systems (en)
skos:notation
  • RIV/49777513:23520/14:43923269!RIV15-TA0-23520___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(TE02000202), S
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
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  • 32782
http://linked.open...ai/riv/idVysledku
  • RIV/49777513:23520/14:43923269
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Navigation; Nonlinear analysis; GPS (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [F767090DB54B]
http://linked.open...v/mistoKonaniAkce
  • Berlin, Germany
http://linked.open...i/riv/mistoVydani
  • Bristol
http://linked.open...i/riv/nazevZdroje
  • Journal of Physics: Conference Series
http://linked.open...in/vavai/riv/obor
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  • Punčochář, Ivo
  • Šimandl, Miroslav
  • Král, Ladislav
  • Škach, Jan
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
issn
  • 1742-6588
number of pages
http://bibframe.org/vocab/doi
  • 10.1088/1742-6596/570/1/012005
http://purl.org/ne...btex#hasPublisher
  • IOP Publishing
http://localhost/t...ganizacniJednotka
  • 23520
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