Safety Analysis for Near Rectilinear Orbit Close Approach Rendezvous in the Circular Restricted Three-Body Problem

We prove in particular that the negative spectrum of H consists, besides the expected absolutely continuous part, of isolated eigenvalues of finite multiplicities

Two scenarios were considered for this transition: direct transfer at the end of the drift using a Lambert’s arc in the CR3BP corrected in the Ephemeris, and

Moreover, in the zero range model, there are energy crossings between universal and efimovian states as a function of R t /a ho (see solid lines in Fig.2a); as we shall see, for

Earth-Moon transfer, low thrust, circular restricted three-body problem, optimal control, minimum time or fuel consumption trajectories, shoot- ing, discrete and

The situation is analogous to the one in Riemannian geometry with cut and conjugate points: Up to some point, the path provides minimizers; then global optimality is lost

We next investigate in more details these stability properties of invariant manifolds of halo and eight-shaped Lissajous orbits (related to the Lagrange point L 1 of the

Next, to bridge a gap between the averaged problem and the works of Henon and Guyot (1970) and Benest (1975), we devote the section 4 to revisit the motion in the rotating frame in

Dans notre série, seuls 2 patients étaient déjà suivis pour sarcoïdose systémique, chez tous les autres patients (88%), elle était inaugurale.. Elle affecte les deux sexes