Endgame problem part 2: multibody technique and the Tisserand-Poincare graph

S Campagnola, RP Russell - Journal of Guidance, Control, and …, 2010 - arc.aiaa.org
THIS paper is the second of a series of two, in which we study the endgame problem in
detail, which is the last part of a trajectory before the insertion maneuver into the science …

Endgame problem part 1: V-infinity-leveraging technique and the leveraging graph

S Campagnola, RP Russell - Journal of Guidance, Control, and …, 2010 - arc.aiaa.org
IN RECENT years both NASA and ESA have studied a variety of mission options to the
Galilean moons at Jupiter and to the moons of Saturn, including Enceladus and Titan. A very …

Optimization of low-energy resonant hopping transfers between planetary moons

G Lantoine, RP Russell, S Campagnola - Acta Astronautica, 2011 - Elsevier
In response to the scientific interest in Jupiter's Galilean moons, NASA and ESA have plans
to send orbiting missions to Europa and Ganymede, respectively. The inter-moon transfers …

Flybys in the planar, circular, restricted, three-body problem

S Campagnola, P Skerritt, RP Russell - Celestial Mechanics and …, 2012 - Springer
An analysis is presented of gravity assisted flybys in the planar, circular, restricted three-
body problem (pcr3bp) that is inspired by the Keplerian map and by the Tisserand-Poincaré …

Tisserand-leveraging transfers

S Campagnola, A Boutonnet… - Journal of Guidance …, 2014 - arc.aiaa.org
Tisserand-leveraging transfers (TILTs) are introduced as a new method for computing low-Δ
v orbit transfers with the help of third-body perturbations. The TILTs can mitigate the costs …

Approaching moons from resonance via invariant manifolds

RL Anderson - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
In this work, the final approach typical of a trajectory traveling from the last resonance of an
endgame scenario in a tour down to a moon is examined within the context of invariant …

Multi-body trajectory design strategies based on periapsis Poincaré maps

DEC Davis - 2011 - search.proquest.com
Incorporating multi-body dynamics into preliminary spacecraft trajectory design expands the
design space and provides trajectory options that may not otherwise be available. However …

Near ballistic halo-to-halo transfers between planetary moons

G Lantoine, RP Russell - The Journal of the Astronautical Sciences, 2011 - Springer
Intermoon transfers are important components of planetary tour missions. However, these
transfers are challenging to design due in part to the chaotic environment created by the …

Trajectory design combining invariant manifolds with discrete mechanics and optimal control

A Moore, S Ober-Blöbaum, JE Marsden - Journal of Guidance, Control …, 2012 - arc.aiaa.org
MANY techniques focus on the design of spacecraft trajectories. For example, invariant
manifolds of the planar circular restricted three-body problem (PCR3BP) can be used to find …

[PDF][PDF] A methodology for robust optimization of low-thrust trajectories in multi-body environments

G Lantoine, RP Russell - 2010 - comet-cnes.fr
Interplanetary space travel has played an important role in the development of our
knowledge of the solar system. For decades, probes have been sent in various destinations …