Log in

Numerical representation of planetary ephemerides

  • Part 6/Representation and Transmission of Results
  • Published:
Celestial mechanics Aims and scope Submit manuscript

Abstract

The Jet Propulsion Laboratory provides high-precision numerically integrated planetary and lunar ephemerides in support of spacecraft navigation and other activities relating to solar system bodies. Hundreds of users around the world have requested copies of the ephemerides. In the interests of compactness and utility, techniques have been developed for (1) the generation of the coefficients of an interpolating polyncmial based on output from the integrator, and (2) transformation of the contents of an ephemeris file to a standard form usable on virtually any computer.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Subscribe and save

Springer+ Basic
EUR 32.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or Ebook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  • Rivlin, T. J.,The Chebyshev Polynomials, John Wiley & Sons, 1974.

  • Newhall, X X, Standish, E. M., and Williams, J. G.: “DE 102: a numerically integrated ephemeris of the Moon and planets spanning forty-four centuries,”Astron. Astrophys. 125, 150–167, 1983.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Newhall, X.X. Numerical representation of planetary ephemerides. Celestial Mechanics 45, 305–310 (1988). https://doi.org/10.1007/BF01229014

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01229014

Keywords

Navigation