Sentence examples for orbital argument from inspiring English sources

Thus, it seems likely that although the molecular orbital argument of Luther[17] may be correct in large part, the fate of the S2O3-like surface group (Fe S S O3) may not result in appreciable free S2O32- in low-pH conditions.

Since the general perturbations method usually uses mean orbital elements as arguments, while the osculating elements play the role of initial conditions for predictions, the relation between the osculating and mean elements has to be determined on the same level of accuracy as that of the theory of motion applied.

Sedna, 2012VP113 and a handful of smaller objects share similar values of a particular orbital characteristic called the "argument of perihelion", which describes the angle that their orbits form with the plane of the solar system.

We show that, in order to maintain the ground track unchanged, the key parameters are the orbital period and the argument of perigee.

Second, the variations in orbital sunshine angles for any given argument of latitude are only a couple of degrees even when the drifting time reaches 500 orbital periods, and the approximation model developed can effectively approach the numerical results.

A study to obtain orbits at constant eccentricity or argument of pericentre has also been carried out, regardless of the orbital plane evolution.

The orbital evolution research shows that they cross the Earth's orbit four times over one cycle of the perihelion argument variations.

Kepler, Galileo, and Descartes all published major books in the first half of the century purporting to resolve this issue,[7] Kepler and Descartes basing their arguments on the physical mechanism each had proposed as governing the orbital motion.

The orbital integration shows that the secular variations in three orbital elements – the ascending node, the argument of perigee, and the mean anomaly at epoch – are larger than the systematic error as results of the relativistic perturbations.

Moreover, when the orbital pole is perpendicular to the perturbing body pole, a prime integral of motion, linking orbit eccentricity and argument of pericentre, has been retrieved.

First, two approximate models for the variations in orbital sunshine angles are developed, one for variations at a given time and the other for variations at a given argument of latitude.