An analytical iterative algorithm for the prediction of special satellite orbit points with the Brouwer orbit theory |
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| Authors: | Robert A Gordon |
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| Institution: | (1) NASA/Goddard Space Flight Center, 20771 Greenbelt, Md., USA |
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| Abstract: | Employing a direct recursive algorithm in relation with analytical theories will yield a considerable saving in computer time, as opposed to simulating a point by point integration through repeated evaluations of the orbit theory. As a case in point, we shall compute the set of osculating orbiting elements corresponding to special events within the revolution of an artificial satellite. |
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