Non-Keplerian orbits for electric sails
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Publication:642305
DOI10.1007/s10569-009-9200-yzbMath1223.70090OpenAlexW2094084976MaRDI QIDQ642305
Giovanni Mengali, Alessandro A. Quarta
Publication date: 26 October 2011
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-009-9200-y
Related Items (9)
On the stability of artificial equilibrium points in the circular restricted three-body problem ⋮ Displaced non-Keplerian orbits using impulsive thrust ⋮ Artificial equilibrium points for a generalized sail in the circular restricted three-body problem ⋮ New families of Sun-centered non-Keplerian orbits over cylinders and spheres. ⋮ Nonlinear dynamics of displaced non-Keplerian orbits with low-thrust propulsion ⋮ Optimal switching strategy for radially accelerated trajectories ⋮ Perturbation solutions to the nonlinear motion of displaced orbits ⋮ Bounded relative motions for formation flying in displaced orbits by low-thrust propulsion ⋮ Determination of thrusts to generate artificial equilibrium points in binary systems with applications to a planar solar sail
Cites Work
- Symmetries in the optimal control of solar sail spacecraft
- Solar sail halo orbits at the Sun-Earth artificial \(L_1\) point
- Planar heliocentric roto-translatory motion of a spacecraft with a solar sail of complex shape
- The existence and stability of families of displaced two-body orbits
- New challenges to trajectory design by the use of electric propulsion and other new means of wandering in the solar system
- Controlled solar sail transfers into near-Sun regions combined with planetary gravity-assist flybys
- Long-term evaluation of three-dimensional heliocentric solar sail trajectories with arbitrary fixed sail setting
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