The invariant manifolds associated with periodic orbits in the vicinity of the collinear libration points in the planar CR3BP have been previously demonstrated as mechanisms for transport. Trajectories that pass between adjoining regions within the zero-velocity curves pass through the invariant manifold tubes. In particular, the invariant manifolds associated with the unstable L1 and L2 periodic libration point orbits may be exploited to construct transit orbits between the interior and exterior regions associated with the zero-velocity curves. In this investigation, periapse Poincaré maps are used to display the manifolds and to distinguish regions of escape and, conversely, regions of long-term capture. Manifold periapse structures are e...
Instead of the two-body problem commonly used in interplanetary trajectory design, also three bodies...
An initial study of techniques to be used in understanding how invariant manifolds are involved in l...
Spacecraft capture trajectories to Lyapunov/Halo periodic orbits of the L1 and L2 points in the rest...
In this investigation, the role of higher-dimensional Poincaré maps in facilitating trajectory desig...
The invariant manifold structures of the collinear libration points for the restricted three-body pr...
The invariant manifold structures of the collinear libration points for the spatial restricted three...
The success of the Genesis spacecraft, as well as the current Artemis mission, continue to generate ...
Space exploration efforts are shifting towards inexpensive and more agile vehicles. Versatility rega...
In the pursuit of establishing a sustainable space economy within the cislunar region, it is vital t...
Incorporating multi-body dynamics into preliminary spacecraft trajectory design expands the design s...
The goal of this lecture is to review several methodologies for the computation of invariant manifol...
When designing spacecraft trajectories, there exist cases where a trade-off between time-of-flight a...
A dynamical understanding of orbits in the Earth-Moon neighborhood that can sustain long-term activi...
Feasibility of operative orbits in the Pluto-Charon system has been investigated in this work. Given...
In this paper a general algorithm for the design of low-energy interplanetary transfers, exploiting ...
Instead of the two-body problem commonly used in interplanetary trajectory design, also three bodies...
An initial study of techniques to be used in understanding how invariant manifolds are involved in l...
Spacecraft capture trajectories to Lyapunov/Halo periodic orbits of the L1 and L2 points in the rest...
In this investigation, the role of higher-dimensional Poincaré maps in facilitating trajectory desig...
The invariant manifold structures of the collinear libration points for the restricted three-body pr...
The invariant manifold structures of the collinear libration points for the spatial restricted three...
The success of the Genesis spacecraft, as well as the current Artemis mission, continue to generate ...
Space exploration efforts are shifting towards inexpensive and more agile vehicles. Versatility rega...
In the pursuit of establishing a sustainable space economy within the cislunar region, it is vital t...
Incorporating multi-body dynamics into preliminary spacecraft trajectory design expands the design s...
The goal of this lecture is to review several methodologies for the computation of invariant manifol...
When designing spacecraft trajectories, there exist cases where a trade-off between time-of-flight a...
A dynamical understanding of orbits in the Earth-Moon neighborhood that can sustain long-term activi...
Feasibility of operative orbits in the Pluto-Charon system has been investigated in this work. Given...
In this paper a general algorithm for the design of low-energy interplanetary transfers, exploiting ...
Instead of the two-body problem commonly used in interplanetary trajectory design, also three bodies...
An initial study of techniques to be used in understanding how invariant manifolds are involved in l...
Spacecraft capture trajectories to Lyapunov/Halo periodic orbits of the L1 and L2 points in the rest...