Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1717436 | Acta Astronautica | 2006 | 7 Pages |
Abstract
We have obtained the expressions of the errors in velocity and position at cut-off, for the hyperbolic and parabolic orbits limited to the coplanar case. The value of ÎÏ, the error in Ï, due to impulse error ÎI, where Ï is any orbital element is assigned by partial differentiations of the relevant equations of hyperbolic and parabolic orbits, as interpreted in two sections of the paper.
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Authors
Osman M. Kamel, Adel S. Soliman,