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- W2368688263 abstract "This paper made a further discussion about the stability of the Triangular Libration points and the possibility to keep a spacecraft around them.Based on the maximum amplitude of the spacecraft during its life,we can find the initial conditions(including the position and the speed).Although the initial deviations of the spacecrafts from the libration points can be very large under the model of circular restricted three-body problem for the large mass ratio μ(μ=0.012) of the earth-moon system,it is nearly impossible to keep a spacecraft around these points without control due to the large perturbations from the sun(the magnitude can reach 2×10-2μ).So control strategy is needed in the lifetime of the spacecrafts.Similar to the orbit control of the GEO,we control the spacecraft longitudinally(control of the semi-major axis) and latitudinally(control of the orbit inclination)." @default.
- W2368688263 created "2016-06-24" @default.
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- W2368688263 date "2008-01-01" @default.
- W2368688263 modified "2023-09-24" @default.
- W2368688263 title "Orbit Drift and Control of the Spacecraft around the Triangular Libration Points in the Earth-Moon System" @default.
- W2368688263 hasPublicationYear "2008" @default.
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