Averaged model to study long-term dynamics of a probe about Mercury

Tresaco, E. ; Carvalho, J.P.S. ; Prado, A.F.B.A. ; Elipe, A. (Universidad de Zaragoza) ; de Moraes, R.V.

Resumen: This paper provides a method for finding initial conditions of frozen orbits for a probe around Mercury. Frozen orbits are those whose orbital elements remain constant on average. Thus, at the same point in each orbit, the satellite always passes at the same altitude. This is very interesting for scientific missions that require close inspection of any celestial body. The orbital dynamics of an artificial satellite about Mercury is governed by the potential attraction of the main body. Besides the Keplerian attraction, we consider the inhomogeneities of the potential of the central body. We include secondary terms of Mercury gravity field from J2 up to J6, and the tesseral harmonics C¯ 22 that is of the same magnitude than zonal J2. In the case of science missions about Mercury, it is also important to consider third-body perturbation (Sun). Circular restricted three body problem can not be applied to Mercury–Sun system due to its non-negligible orbital eccentricity. Besides the harmonics coefficients of Mercury’s gravitational potential, and the Sun gravitational perturbation, our average model also includes Solar acceleration pressure. This simplified model captures the majority of the dynamics of low and high orbits about Mercury. In order to capture the dominant characteristics of the dynamics, short-period terms of the system are removed applying a double-averaging technique. This algorithm is a two-fold process which firstly averages over the period of the satellite, and secondly averages with respect to the period of the third body. This simplified Hamiltonian model is introduced in the Lagrange Planetary equations. Thus, frozen orbits are characterized by a surface depending on three variables: the orbital semimajor axis, eccentricity and inclination. We find frozen orbits for an average altitude of 400 and 1000 km, which are the predicted values for the BepiColombo mission. Finally, the paper delves into the orbital stability of frozen orbits and the temporal evolution of the eccentricity of these orbits.

Idioma: Inglés

DOI: 10.1007/s10569-017-9801-9

Año: 2018

Publicado en: Celestial Mechanics and Dynamical Astronomy 130, 2 (2018), 9 [26 pp.]
ISSN: 0923-2958

Factor impacto JCR: 1.837 (2018)

Categ. JCR: MATHEMATICS, INTERDISCIPLINARY APPLICATIONS rank: 42 / 104 = 0.404 (2018) - Q2 - T2
Categ. JCR: ASTRONOMY & ASTROPHYSICS rank: 38 / 69 = 0.551 (2018) - Q3 - T2

Factor impacto SCIMAGO: 0.781 - Applied Mathematics (Q1) - Astronomy and Astrophysics (Q1) - Space and Planetary Science (Q1) - Mathematical Physics (Q1) - Modeling and Simulation (Q1) - Computational Mathematics (Q1)

Financiación: info:eu-repo/grantAgreement/ES/MINECO/2013-44217-R

Tipo y forma: Artículo (PostPrint)

Área (Departamento): Área Matemática Aplicada (Dpto. Matemática Aplicada)