dc.contributor.author |
Lantoine, Gregory |
|
dc.contributor.author |
Broschart, Stephen B. |
|
dc.contributor.author |
Grebow, Daniel J. |
|
dc.date.accessioned |
2013-11-19T18:03:20Z |
|
dc.date.available |
2013-11-19T18:03:20Z |
|
dc.date.issued |
2013-08-12 |
|
dc.identifier.citation |
AAS/AIAA Astrodynamics Specialist Conference, Hilton Head, South Carolina, August 2013 |
en_US |
dc.identifier.clearanceno |
13-1603 |
|
dc.identifier.uri |
http://hdl.handle.net/2014/44020 |
|
dc.description.abstract |
Global mapping campaigns are part of most primitive body exploration missions. However, designing a mapping orbit without station keeping maneuvers is challenging due to the highly perturbed environment near small bodies. In this paper, we present a new design methodology to support mapping campaigns using ‘quasi-terminator’ orbits, a class of quasi-periodic orbits that exist in the vicinity of the well-known terminator orbits. The inherent stability of quasi-terminator trajectories and their wide variety of viewing geometries make them a very compelling option for mapping campaigns. A high-fidelity test case solution is also presented to prove the existence of these mapping orbits in full ephemeris. |
en_US |
dc.description.sponsorship |
NASA/JPL |
en_US |
dc.language.iso |
en_US |
en_US |
dc.publisher |
Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013. |
en_US |
dc.subject |
quasi-terminator |
en_US |
dc.subject |
quasi-periodic orbits |
en_US |
dc.title |
Mission design for global mapping orbits at primitive bodies |
en_US |
dc.type |
Preprint |
en_US |