Proper elements for highly inclined asteroidal orbits
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Publication:1804279
DOI10.1007/BF00693091zbMath0825.70061OpenAlexW1967772985MaRDI QIDQ1804279
Anne Lemaitre, Alessandro Morbidelli
Publication date: 28 November 1995
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf00693091
Computational methods for problems pertaining to mechanics of particles and systems (70-08) Celestial mechanics (70F15)
Related Items (6)
Proper elements for space debris ⋮ Proper elements for resonant planet-crossing asteroids ⋮ About averaging procedures in the problem of asteroid motion ⋮ Dynamics of highly eccentric and highly inclined space debris ⋮ Old perturbative methods for a new problem in celestial mechanics: the space debris dynamics ⋮ Are the analytical proper elements of asteroids still needed?
Cites Work
- Secular perturbation theory and computation of asteroid proper elements
- A semi-numerical perturbation method for separable Hamiltonian systems
- Secular resonances in the asteroid belt: Theoretical perturbation approach and the problem of their location
- Asteroid long-periodic perturbations: the second order Hamiltonian
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