JPL Technical Report Server

On the detection of energetically efficient trajectories for spacecraft

Show simple item record

dc.contributor.author Dellnitz, Michael
dc.contributor.author Junge, Oliver
dc.contributor.author Lo, Martin
dc.contributor.author Thiere, Bianca
dc.date.accessioned 2007-11-06T01:16:56Z
dc.date.available 2007-11-06T01:16:56Z
dc.date.issued 2001-07-30
dc.identifier.citation AAS/AIAA Astrodynamics Specialists Conference, Quebec City, Canada, July 30 - August 2, 2001 en
dc.identifier.clearanceno 01-1628
dc.identifier.uri http://hdl.handle.net/2014/40517
dc.description.abstract We propose a new method for the detection of energy-efficient trajectories for spacecraft. Via a so called target-shooting approach a pseudo-orbit between the relevant points in space is constructed in a simple model of the problem. This approximate trajectory is meant to serve as input for a more sophisticated direct method in order to compute a true trajectory in the full model. We demonstrate the applicability of the new method by considering the redesign of part of the trajectory of the NASA/JPL Genesis discovery mission. en
dc.description.sponsorship NASA/JPL en
dc.format.extent 271178 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2001. en
dc.subject halo orbits en
dc.subject target shooting en
dc.subject Genesis mission en
dc.title On the detection of energetically efficient trajectories for spacecraft en
dc.type Preprint en


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search


Browse

My Account