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Please use this identifier to cite or link to this item:
http://hdl.handle.net/2014/9375
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| Title: | System engineering challenges of real-time simulation for Mars SmartLander entry, descent, and landing |
| Authors: | Martin, B. J.
Henriquez, D. A.
Balaram, B.
Sohl, G. A.
Pomerantz, M. I. |
| Issue Date: | 6-Aug-2002 |
| Citation: | AIAA Conference on Atmospheric Flight Mechanics
Monterey, CA, USA |
| 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. |
| URI: | http://hdl.handle.net/2014/9375 |
| Appears in Collections: | JPL TRS 1992+
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