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Evasive Maneuvers in Space Debris Environment and Technological Parameters
2012
Mathematical Problems in Engineering
We present a study of collisional dynamics between space debris and an operational vehicle in LEO. We adopted an approach based on the relative dynamics between the objects on a collisional course and with a short warning time and established a semianalytical solution for the final trajectories of these objects. Our results show that there are angular ranges in 3D, in addition to the initial conditions, that favor the collisions. These results allowed the investigation of a range of
doi:10.1155/2012/126521
fatcat:4v23monwo5asfpqsiebyf7of3m