Interplanetary Transfer Trajectories Using the Invariant Manifolds of Halo Orbits
Throughout the history of interplanetary space travel, the Newtonian dynamics of the two-body problem have been used to design orbital trajectories to traverse the solar system. That is, that a spacecraft orbits only one large celestial body at a time. These dynamics have produced impressive interpl...
| Main Author: | |
|---|---|
| Format: | Others |
| Published: |
DigitalCommons@CalPoly
2018
|
| Subjects: | |
| Online Access: | https://digitalcommons.calpoly.edu/theses/1853 https://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=3173&context=theses |