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System engineering challenges of real-time simulation for Mars SmartLander entry, descent, and landing

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dc.contributor.author Martin, B. J. en_US
dc.contributor.author Henriquez, D. A. en_US
dc.contributor.author Balaram, B. en_US
dc.contributor.author Sohl, G. A. en_US
dc.contributor.author Pomerantz, M. I. en_US
dc.date.accessioned 2004-09-17T06:44:39Z
dc.date.available 2004-09-17T06:44:39Z
dc.date.issued 2002-08-06 en_US
dc.identifier.citation AIAA Conference on Atmospheric Flight Mechanics en_US
dc.identifier.citation Monterey, CA, USA en_US
dc.identifier.clearanceno 02-1571 en_US
dc.identifier.uri http://hdl.handle.net/2014/9375
dc.description.abstract The Jet Propulsion Laboratory (JPL) is developing a high-fidelity, real-time spacecraft simulator for Entry, Descent and Landing (EDL) on planetary and small bodies. This simulator, DSENDS (Dynamics Simulator for Entry, Descent and Surface landing), is an EDL-specific extension of the JPL Darts/Dshell multi-mission spacecraft dynamics and devices simulation toolkit which is in use by missions such as Cassini, Galileo, SIM, and Starlight. en_US
dc.format.extent 3726267 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Dshell EDL simulator en_US
dc.title System engineering challenges of real-time simulation for Mars SmartLander entry, descent, and landing en_US


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