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Book Chapter

Satellite in Real (Perturbed) Orbit

  • Capderou M
Springer International Publishing, (2014), 163-244
DOI: 10.1007/978-3-319-03416-4_6
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Abstract

We first examine all the forces (perturbing forces) that separate the real motion of the satellite from its theoretical ideal motion (Keplerian). We the apply the theories of Lagrange's equations of the perturbing method to determine the changes to each of the orbital elements.

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APA

Capderou, M. (2014). Satellite in Real (Perturbed) Orbit. In Handbook of Satellite Orbits (pp. 163–244). Springer International Publishing. https://doi.org/10.1007/978-3-319-03416-4_6

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