Luni-solar effects of geosynchronous orbits at the critical inclination
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Publication:1311629
DOI10.1007/BF00692471zbMath0820.70013OpenAlexW4230599020MaRDI QIDQ1311629
Alessandro Morbidelli, Fabienne Delhaise
Publication date: 17 September 1995
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf00692471
Dynamical aspects of finite-dimensional Hamiltonian and Lagrangian systems (37J99) Perturbations of finite-dimensional Hamiltonian systems, normal forms, small divisors, KAM theory, Arnol'd diffusion (37J40) Celestial mechanics (70F15) Orbital mechanics (70M20)
Related Items (8)
The dynamical structure of the MEO region: long-term stability, chaos, and transport ⋮ Analytical development of the lunisolar disturbing function and the critical inclination secular resonance ⋮ Extension of the critical inclination ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations ⋮ Towards a sustainable exploitation of the geosynchronous orbital region ⋮ Analytical study of the resonance caused by solar radiation pressure on a spacecraft ⋮ Families of frozen orbits of lunar artificial satellites ⋮ Dynamics of artificial satellite orbits with tesseral resonances including the effects of luni- solar perturbations
Cites Work
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- A semi-numerical perturbation method for separable Hamiltonian systems
- On analytic modeling of Lunar perturbations of artificial satellites of the Earth
- The critical inclination problem ? 30 years of progress
- Orbits near critical inclination, including lunisolar perturbations
- Lunar perturbations of artificial satellites of the earth
- A note on Hansen's coefficients in satellite theory
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