Formation flying solar-sail gravity tractors in displaced orbit for towing near-Earth asteroids
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Publication:642304
DOI10.1007/s10569-009-9211-8zbMath1223.70086OpenAlexW2159003399MaRDI QIDQ642304
Sheng-Ping Gong, Jun-Feng Li, He-Xi Baoyin
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/s10569-009-9211-8
formation flyingsolar sailasteroid deflectiongravitational tractorNEO deflection-displaced orbit near an asteroid
Related Items (5)
Displaced non-Keplerian orbits using impulsive thrust ⋮ Artificial equilibrium points for a generalized sail in the circular restricted three-body problem ⋮ Formation around planetary displaced orbit ⋮ On the deflection of asteroids with mirrors ⋮ Solar sail periodic orbits in the elliptic restricted three-body problem
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