| Visual Analysis of a Simulated
Plasma Plume and its Interaction with the Deep Space 1 Spacecraft
Visual Analysis of a Simulated Plasma Plume and its Interaction with the Deep Space 1 Spacecraft
Many limiting factors of Electric Propulsion (EP) are slow to manifest, and thus are hard and expensive to discover using vacuum tank tests. Computer simulation uses elementary laws of plasma physics to push the particles making up the fluid. As such, effects like the grid erosion, plasma coating or spacecraft charging can be discovered in a fraction of the time needed by a vacuum tank experiment by performing a computer simulation.
Progress (as of 03/09/2003)
My undergraduate research consists of working with the other members of the Computational Advanced Propulsion Lab (Cap Lab) on simulating plasma for a variety of surface geometry conditions. Currently, the input conditions are entered using analytical expressions, but the ongoing work consists of generating a universal code. This code is being developed as a joint project with MIT, under the sponsorhip of the Air Force Research Labs. The code will be able to read in a geometry definition file with the associated potential values, solve the electric field and perfom the simulation.
Furthermore, I am developing the Cap Lab Virtual Testing Environment, or capVTE. capVTE is a cross-platform visualization software, which uses the Visualization Toolkit for its object rendering. The objective of the program is to create an immersed visualization platform, allowing the user to study data on both a workstation and in the CAVE. Currently, it is possible to export .iv files which can then be explored using diversifly. However, after completion, capVTE will directly interact with the CAVE. This will allow the user to adjust the visualization parameters from the CAVE by using the wand interface. Completion of the fully immersed version of capVTE is however outside the scope of this project.
The main objectives of the project are to:
Generate an easy to understand multimedia presentation outlining the physical models used in computer plasma simulation.
Use Tecplot and capVTE to explore the data from a simulation of the Deep Space 1 thruster. The two software packages will be explored and their respective strengths will be compared. The electric potential and charge density will be examined. The time-varying velocity distribution of the emmited ions will be animated.
Discuss the results with students at MIT as well as interested parties at AFRL by employing the Collaborative Toolkit for Diverse.
The data analysis will be performed using Tecplot and capVTE. The supporting software will include the diverse package, and a VRML web pluggin (such as vrweb). Animation of the vector field will be captured using a screen-capture software, but the specific software has not been identified yet.