Time Transfer Using Geostationary Satellites: Implementation of Kalman Filter,

Abstract

Since 1988, various experiments 1, 2, 3, 4 have shown that the TV signals transmitted by direct TV satellites may easily be used to perform time transfers at the level of a few tens of nanoseconds, the main source of error being the uncertainty on the satellite position. We first present the two methods used in our experiment to reduce the effects of the satellite residual motion : the first one consists in estimating the longitude variations of the satellite and then using this information to improve other measurements. This allows to reduce the uncertainty to values between 9 and 50 nanoseconds according to the position of the involved stations. In the second method we deter-mine the satellite position by using the data collected by three calibrated stations. Time transfer between each of these stations and a fourth one has been shown to be achievable at the precision level of ten nanoseconds. A new approach based on the use of a Kalman filter is proposed in order to take account the dynamics of the geostationary satellite. The precisions on orbital elements and clock differences and rates determination given by the first simulated applications of the Kalman filter are presented and compared to those obtained by the other methods.

Document Details

Document Type
Technical Report
Publication Date
Dec 02, 1993
Accession Number
ADP009111

Entities

People

  • Florian Meyer

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Clocks
  • Filters
  • Geosynchronous Satellites
  • Kalman Filters
  • Measuring Instruments
  • Nanosecond Time
  • Orbital Elements
  • Precision
  • Time Intervals
  • Uncertainty

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Positioning, Navigation, and Timing (PNT) Technology.

Technology Areas

  • Space
  • Space - Orbital Debris