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CELESTIAL MECHANICS, PART I
Contents:
  1. Systems Thinking, : Managing Chaos and Complexity: A Platform for Designing Business Architecture
  2. Relative Equilibria in the Spherical, Finite Density Three-Body Problem
  3. Steels: Metallurgy and Applications, Third Edition
  4. Documento senza titolo
Orbital Dynamics Part 57 -- The N Body Problem

Phys, n. Abatangelo and S. Abatangelo, V. Felli and S. Terracini, N. Tzvetkov and N. Barutello, S.

Systems Thinking, : Managing Chaos and Complexity: A Platform for Designing Business Architecture

PDE, 49 , no. Boureanu, B. Noris, S. Berestycki, S. Terracini, K. Wang and J. Dierential Equations, , n.

Relative Equilibria in the Spherical, Finite Density Three-Body Problem

PDE 45, n. Felli, A. Ferrero and S. Noris, H. Tavares Terracini S. Verzini and T. Partial Dierential Equations 36 , no. Fixed Point Theory Appl. Noris and Terracini S. Helffer, T. Hoffmann-Ostenhof and S. International Mathematical Series. Tavares, Terracini S. Felli, E. Marchini, and S. Meyers Ed. Barutello, Ferrario D. Rational Mech. Anal, n. Arioli, V. Barutello and S. Phys, Felli, V. Partial Dierential Equations 31 , no.


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Felli V. Arioli G. Phys, , n. Conti M. Bonheure, L. Sanchez, M. Tarallo and S. Functional Analysis, Conti M. Serra, E.

Lincei Cl. Lincei 9 Mat. Dierential Equations , no. Dierential Equations 7 , no. Habets, L. Dierential Equations , Serra E. TMA 41 , Arioli G. Nonlinearity 13 , Conti M. Part II: the forced case.

Steels: Metallurgy and Applications, Third Edition

Tarallo M. I Math. Nonlinear Anal. A: Theory Methods, Montecchiari P. Paris S?

Documento senza titolo

Partial Dierential Equations 5 , no. Transfer to near-Earth asteroids from a lunar orbit via Earth flyby and direct escaping trajectories. Energy analysis and trajectory design for low-energy escaping orbit in Earth—Moon system. A survey of different classes of Earth-to-Moon trajectories in the patched three-body approach.

Initial condition maps of subsets of the circular restricted three-body problem phase space.

Adjoints estimation methods for impulsive Moon-to-Earth trajectories in the restricted three-body problem. Approaching Moons from Resonance via Invariant Manifolds. Study of the gravitational capture of a spacecraft by Jupiter. Spatial approaches to moons from resonance relative to invariant manifolds.

Transfer to long term distant retrograde orbits around the Moon. On the construction of low-energy cislunar and translunar transfers based on the libration points. Survey of Ballistic Transfers to the Lunar Surface. Flybys in the planar, circular, restricted, three-body problem. Trajectory evolution in the multi-body problem with applications in the Saturnian system. Transition Boundaries at the Collinear Libration Points.

Control of Lagrange point orbits using solar sail propulsion. Optimized transfer trajectories in the earth-moon system. Hamilton—Jacobi modelling of stellar dynamics. Connecting orbits and invariant manifolds in the spatial restricted three-body problem.