Celestial mechanics

, Volume 2, Issue 1, pp 21–40 | Cite as

Numerical verification of analytic expressions for the perturbations due to an arbitrary zonal harmonic of the geopotential

  • Anthony G. Lubowe
  • Robert E. Jenkins
Article

Abstract

Expressions are given for the first order node-to-node perturbations in the orbital elements of a satellite due to an arbitrary zonal harmonic of the geopotential. Accurate and efficient procedures for computing such perturbations are necessary for orbit determination methods which will fully utilize the highly accurate observations now available.

Comparison with a double precision numerical integration is made for an intermediate altitude satellite, TELSTAR I. (Second order perturbations due to the second harmonic, derived elsewhere, are included, as are the first order perturbations due to the zonals through fourteenth order.) Discrepancies in semi-major axis after 1 period are of the order of 0.1 mm. Discrepancies in timing are of the order of 0.03 msec. A detailed discussion of computational efficiency is included.

Keywords

Computational Efficiency Determination Method Orbital Element Orbit Determination Double Precision 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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Copyright information

© D. Reidel Publishing Company 1970

Authors and Affiliations

  • Anthony G. Lubowe
    • 1
  • Robert E. Jenkins
    • 2
  1. 1.Bell Telephone Laboratories, Inc.WhippanyUSA
  2. 2.Applied Physics LaboratoryThe Johns Hopkins UniversitySilver SpringUSA

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