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- W2348644121 abstract "Taking the advantage of the 'cluster' character of the motion,a two-stage plan strategy for satellite formation maneuvering is presented.The first stage is to plan the maneuvering trajectory of the reference satellite,the secondly stage is to plan the trajectories of the concomitant satellites.The trajectory of the reference satellite is optimized and validated by Gauss Pseudospectral Method(GPM).Based on the reference trajectory,the feasible flying area of the concomitant satellites are determined according to the path constraints.The trajectories of the concomitant satellites are in the feasible flying area,connecting the initial states and the final states of the formation.And the control variables are deduced from the trajectories based on the dynamic inversion method.Lastly,the feasibly of the trajectories of the concomitant satellites is analyzed.And the optimal condition of the results is validates.Simulation results show the approach can reduce the computing amount,and can satisfy all the requirements of the satellite formation maneuvering mission." @default.
- W2348644121 created "2016-06-24" @default.
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- W2348644121 date "2009-01-01" @default.
- W2348644121 modified "2023-09-23" @default.
- W2348644121 title "Study of a Planning Approach for Satellite Formation Maneuvering" @default.
- W2348644121 hasPublicationYear "2009" @default.
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