Accurate computation of highly eccentric satellite orbits

DOI10.1007/BF01229121zbMath0303.70045MaRDI QIDQ4058275

G. Janin

Publication date: 1974

Published in: Celestial Mechanics (Search for Journal in Brave)

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (13)

Geometrical definition of a continuous family of time transformations generalizing and including the classic anomalies of the elliptic two-body problem ⋮ Geometrical definition of a continuous family of time transformations on the hyperbolic two-body problem ⋮ CMMSE: Study of a new symmetric anomaly in the elliptic, hyperbolic, and parabolic Keplerian motion ⋮ A study about the integration of the elliptical orbital motion based on a special one-parametric family of anomalies ⋮ A note on the use of generalized Sundman anomalies in the numerical integration of the elliptical orbital motion ⋮ A new bi-parametric family of temporal transformations to improve the integration algorithms in the study of the orbital motion ⋮ Length of arc as independent argument for highly eccentric orbits ⋮ Remarks on the numerical integration of near-parabolic orbits ⋮ Accurate integration of geostationary orbits with Burdet's focal elements ⋮ The intermediate anomaly ⋮ Keplerian motion and gyration ⋮ Time elements in Keplerian orbital elements ⋮ DROMO propagator revisited

Cites Work

• Numerical stabilization of the differential equations of Keplerian motion
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