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- W2358609940 abstract "Relative motion between spacecrafts is researched based on kinematics models.On the basis of simplifing the relative motion model,relative motion kinematics equations for the J2 perturbed orbit are derived,which are based on the model described by using argument of latitude and mean anomaly.In addition,simulation and analysis for relative trajectories are researched.Simulation results for relative trajectories corresponded with analysis for equtions derived in this paper,so both the method to build a model and the model built could be used for design of the space mission.The simulation results show that more accurate equations of relative motion can be obtained by using the kinematics method,and equations under perturbations will be more simple." @default.
- W2358609940 created "2016-06-24" @default.
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- W2358609940 date "2011-01-01" @default.
- W2358609940 modified "2023-09-24" @default.
- W2358609940 title "Research on kinematics model of relative motion between spacecrafts" @default.
- W2358609940 hasPublicationYear "2011" @default.
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