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Erschienen in:
2014 | OriginalPaper | Buchkapitel
On Spacecraft Relative Orbital Motion Based on Main-Flying Direction Method
verfasst von : Yanchao Sun, Huixiang Ling, Chuanjiang Li, Guangfu Ma, Wenrui Zhao
Erschienen in: Intelligent Computing Methodologies
Verlag: Springer International Publishing
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This paper introduces an analysis of a relative orbit control problem that how to let the tracking spacecraft be in the range of a small angle which is outward from the non-cooperative target spacecraft’s field of view, and at the same time satisfy the requirement of flight time and distance. This analysis is called “main-flying direction” analysis method. Based on this method, we provide a design method of the relative orbit in the fluttering mode that the tracking spacecraft flies in its own orbit after it enters into the spatial range relevant to the target spacecraft. This design method of solving the relative orbit control problem is demonstrated by simulations. The analysis thought and the calculation of this method are simple, and it avoids some disadvantages in other methods, such as the direction limitation of the field of view, attitude and orbit control coupling, etc.