meetings - Space Flight Mechanics Committee
meetings - Space Flight Mechanics Committee
meetings - Space Flight Mechanics Committee
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16:15 AAS Verification and Validation of the MSL/Curiosity Rover Entry Descent and<br />
13-464 Landing System<br />
Richard Kornfeld, NASA / Caltech JPL; Ravi Prakash, NASA / Caltech JPL; Allen<br />
Chen, NASA / Caltech JPL; Ann Devereaux, NASA / Caltech JPL; Martin Greco,<br />
NASA / Caltech JPL; Corey Harmon, NASA / Caltech JPL; Devin Kipp, NASA /<br />
Caltech JPL; Alejandro San Martin, NASA / Caltech JPL; Steven Sell, NASA /<br />
Caltech JPL; Adam Steltzner, NASA / Caltech JPL<br />
On August 5/6, 2012, the Curiosity rover successfully touched down on the Martian surface<br />
setting off the most ambitious surface exploration of this planetary body. Preceding this<br />
significant step were years of design, development and testing of the Curiosity Entry,<br />
Descent and Landing (EDL) system to prepare for the most complex landing endeavor ever<br />
attempted at Mars. This paper discusses the approach and implementation of the overall<br />
EDL verification and validation (V&V) program. The lessons learned and conclusions<br />
described herein can serve as a pathfinder for the EDL system testing approach and<br />
implementation of future Mars landed missions.<br />
16:35 AAS Managing Complexity in the MSL/Curiosity Entry, Descent, and Landing<br />
13-463 <strong>Flight</strong> Software and Avionics Verification and Validation Campaign<br />
Aaron Stehura, NASA / Caltech JPL; Matthew Rozek, NASA / Caltech JPL<br />
The complexity of the Mars Science Laboratory (MSL) mission presented the Entry,<br />
Descent, and Landing systems engineering team with many challenges in its Verification<br />
and Validation (V&V) campaign. This paper describes some of the logistical hurdles related<br />
to managing a complex set of requirements, test venues, test objectives, and analysis<br />
products faced by the authors as they implemented a specific portion of V&V to test the<br />
interaction of flight software with the MSL avionics. Application-specific solutions to these<br />
problems are presented herein, which can be generalized to other space missions and to<br />
similar formidable systems engineering problems.<br />
Page 90<br />
23 rd AAS / AIAA <strong>Space</strong> <strong>Flight</strong> <strong>Mechanics</strong> Meeting