Sentence examples for both orbits was obtained from inspiring English sources

For the areal-average, a coefficient of correlation (R) of ∼0.61 and ∼0.72 for the morning and afternoon orbits, respectively, and a centered root mean square difference (cRMSD) of ∼0.04 m3 m−3 for both orbits was obtained.

A contrast-enhanced CT of the orbits was obtained, which showed right preseptal swelling, as well as marked enlargement of the right lacrimal gland with an area of central low attenuation, and swelling of the adjacent extra-ocular muscles (Fig. 1).

The errors results and analysis for SSO (the Sun synchronous orbit) typical orbits are obtained.

Almost periodic orbits are obtained, but the model in the searched flapping-of-wing flight is unstable.

Additionally, two families of equatorial orbits are obtained at a wide range of distances: from far away to nearby.

To show the effect of the oblateness, the planar Lyapunov family emanating from the Lagrangian points and three-dimensional halo orbits are obtained by the numerical continuation method.

A new existence of hyperbolic orbits is obtained for a class of singular Hamiltonian systems with prescribed energies by taking the limit for a sequence of approximate solutions.

We construct a variational framework of the above-mentioned problem, and some new results on the existence of a homoclinic orbit or an unbounded sequence of homoclinic orbits are obtained by using the mountain pass lemma and the symmetric mountain pass lemma, respectively.

The steady-state orbits are obtained by requiring the double derivates to be zero, this will yield x 10 = x ˙ 10 = x ˙ 20 = 0, x 20 = - λ Ω w v 30 ω i 2 - ω b 2 γ | | - 2 + k w v 30 Ω 0 - k w v 30 - 1, x ˙ 30 = const.

This type of orbit is obtained for an interval of μ values.

The full-flight trajectory including transfer trajectory from lunar orbit to Sun Earth L2 region and target Lissajous orbit is obtained by the differential correction method.