The use of an almost unknown orbital propriety, the quasiconstancy of angular velocity around the second focus, leads to a non iterative and by hand method of updating the position of a satellite in low-eccentric orbit.

The second focus method

;
2004

Abstract

The use of an almost unknown orbital propriety, the quasiconstancy of angular velocity around the second focus, leads to a non iterative and by hand method of updating the position of a satellite in low-eccentric orbit.
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Utilizza questo identificativo per citare o creare un link a questo documento: http://hdl.handle.net/11367/26219
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