Article ID Journal Published Year Pages File Type
1717436 Acta Astronautica 2006 7 Pages PDF
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 Δσ, the error in σ, due to impulse error ΔI, where σ 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.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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