dc.contributor.author |
Scheeres, D. J. |
en_US |
dc.date.accessioned |
2004-09-30T05:53:22Z |
|
dc.date.available |
2004-09-30T05:53:22Z |
|
dc.date.issued |
1996-07-29 |
en_US |
dc.identifier.citation |
San Diego, California, USA |
en_US |
dc.identifier.clearanceno |
96-0793 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/25269 |
|
dc.description.abstract |
This paper discusses and describes the dynamics and control of a spacecraft orbiting close to or landing on an asteroid or comet. The paper presents analytical and numerical results which illustrate the challenges facing near-asteroid orbiters. |
en_US |
dc.format.extent |
2936888 bytes |
|
dc.format.mimetype |
application/pdf |
|
dc.language.iso |
en_US |
|
dc.subject.other |
near-asteroid orbiters orbit determination orbit control orbital dynamics |
en_US |
dc.title |
Close Proximity and Landing Orbits at Asteroids |
en_US |