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SMC-IT 2011
TOPICS OF INTEREST

Reliable Software

Autonomy & Automation

CubeSat Software

Space Cybersecurity

Robotics Software

Engineering Design Tools

Fault Management

Real-Time Embedded Systems

Machine Vision

Image Processing

Flight Computing

Novel Applications

Mission Architecture Design

Operations Technologies

Middleware Services

Knowledge Management

Integrated System Health Management

Astronaut Support IT

Science Software Applications

On-board vs Ground Computing

Space Communications

Smart Instruments

Mission Assurance IT

Software Architectures & Tools


SCHEDULE

OCTOBER 1, 2010
Call for Full Papers and Mini-Workshop Summaries

NOVEMBER 1, 2010
Author Submission Website Open

DECEMBER 31, 2010
Call for Full Papers and Mini-Workshop Summaries

MARCH 20, 2011
Author Acceptance Notification

MAY 19, 2011
Early Bird Registration Opens

MAY 19, 2011
Preliminary Program Announced

MAY 20, 2011
Camera Ready Manuscripts Due (incorporating reviewer comments) for upload to the IEEE CPS website

JULY 1, 2011
Regular Registration Opens

AUGUST 2 - 4, 2011
Conference


SMC-IT 2011 TOURS
(August 5, 2011)

USGS, Menlo Park Tour


 

NASA Ames Research Center Tour


 

Computer History Museum


 

Intel Museum (on your own)
Intel Museum


 

Hiller Aviation Museum

Ames Wind TunnelCrowne Plaza Cabana HotelComputer-History-MuseumAmes Pleiades SupercomputerIntel 80 Core Teraflops Research Wafer
NOTE: To receive future announcements, please send a blank email to:
smc-it-join@smc-it.org

MINI-WORKSHOP ON

APPLIED MODELING AND SIMULATION OF SPACE VEHICLES USING SUPERCOMPUTERS

CALL FOR PAPERS

Held in conjunction with the Fourth International Conference on Space Mission Challenges for Information Technology (SMC-IT-2011), August 2 - 4, 2011, in Palo Alto, California, USA.

Abstract:

This session will focus on large-scale applied modeling and simulation that supports critical engineering applications, decisions, and objectives for NASA missions. Utilizing NASA's high-end computing resources, such as those at NASA's Advanced Supercomputing Facility, the contributed papers provide a diverse spectrum of advanced computational analysis that quantify and explain the complex physical processes and phenomena that are crucial to the performance of NASA systems and technologies. The focus is on computational fluid dynamics simulations, but the session is open to all simulations that require high-fidelity algorithms, high-performance supercomputers, and information technologies.  Primary applications expected for this session include aerodynamic and aero-thermal simulations for the development of next-generation launch vehicles and space exploration vehicles. Specifically, high-fidelity simulations of the launch environment, ascent, entry, descent, and landing are anticipated. The session is also open to authors presenting the development of new computational tools and techniques to address the unique challenges and questions that arise in NASA's innovative projects.  Examples of anticipated topics include: the development of best practices for simulating heavy-lift vehicles during launch and ascent, analysis of plume effects during ascent, optimization techniques applied  to the design of next-generation vehicles, development of  high-performance high-accuracy simulation tools, simulations of engine  throttling, simulations of stage separation, simulations of wind tunnel  test conditions, and best practices for acoustics simulations in the  launch environment.  As NASA embarks on an ambitious new path to develop a next-generation space launch system (SLS) both swiftly and affordably, cutting-edge analysis tools and simulations will be critical to streamlining the design process while also ensuring the highest possible performance and safety standards. This session will highlight the tools and simulations that will make this possible.

Organization:

Session Chair(s): Cetin C. Kiris, Ph.D., NASA Ames Research Center, Cetin.C.Kiris@nasa.gov