Orbits near critical inclination, including lunisolar perturbations

Details Orbits near critical inclination, including lunisolar perturbations Orbits near critical inclination, including lunisolar perturbations

Aug 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976aaas.confr....h&link_type=abstract

American Institute of Aeronautics and Astronautics and American Astronautical Society, Astrodynamics Conference, San Diego, Cali

Astronomy and Astrophysics

Astronomy

Angular Distribution, Lunar Gravitational Effects, Orbit Perturbation, Perigees, Solar Gravitation, Eccentricity, Hamiltonian Functions, Inclination, Von Zeipel Method, Zonal Harmonics

Scientific paper

A theory is advanced describing the long-period motion of the perigee of a near-earth orbiter near the critical inclination of 63 deg 26 min 6 sec for large and small eccentricities. Lunisolar perturbations are included in the averaged Hamiltonian, as well as contributions from all the known zonal harmonics to date. Results are discussed using three different earth models.

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