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Kinematic and highly reduced-dynamic LEO orbit determination for gravity field estimation

  • University of Bern

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

9 Scopus citations

Abstract

Kinematic positions of low Earth orbiting satellites equipped with spaceborne GPS receivers are widely used as input for subsequent gravity field estimation procedures. Positions relying on reduceddynamic orbit determination, however, are often considered as inappropriate for this task, because they depend to some extent on the gravity field model underlying the orbit estimation. We review the principles of reduced-dynamic orbit determination and give the mathematical background for a very efficient estimation scheme of reduced-dynamic satellite trajectories using least-squares methods. Simulated as well as real data from the CHAMP GPS receiver are used to show the equivalence of kinematic and reduceddynamic orbits in the kinematic limit and to present a highly reduced-dynamic orbit determination scheme as an alternative to kinematic point positioning.

Original languageEnglish
Title of host publicationDynamic Planet
Subtitle of host publicationMonitoring and Understanding a Dynamic Planet with Geodetic and Oceanographic Tools - lAG Symposium
Pages354-361
Number of pages8
DOIs
StatePublished - 2007
Externally publishedYes
EventIAG Symposium on Dynamic Planet: Monitoring and Understanding a Dynamic Planet with Geodetic and Oceanographic Tools - Cairns, QLD, Australia
Duration: 22 Aug 200526 Aug 2005

Publication series

NameInternational Association of Geodesy Symposia
Volume130
ISSN (Print)0939-9585

Conference

ConferenceIAG Symposium on Dynamic Planet: Monitoring and Understanding a Dynamic Planet with Geodetic and Oceanographic Tools
Country/TerritoryAustralia
CityCairns, QLD
Period22/08/0526/08/05

Keywords

  • Kinematic orbit determination
  • Low Earth orbiter
  • Reduced-dynamic orbit determination

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