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| || Update code to SPC v3.1 || Incorporate the improvements that Gaskell added to SPC during the Rosetta mission. Supports pole wobble more effectively || Action || 16 weeks || SPOC || | |
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| || Wiki version || Update Wiki with version number on all modules || Low || 2 weeks || Palmer || | || || || Low || 2 weeks || Palmer || |
SPC Test Wish List
Here are the tests that are desired to be done during Phase E
Test |
Description |
Priority |
Effort |
Customer |
Action |
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Pole Wobble |
Test the new modules that were changed in support of the Rosetta mission to support Pole Wobble. Std error. |
Action |
12 weeks prep + 12 weeks |
SPOC |
Shape 3 redo |
Run Approach phase testing to see if the improved procedures performs as well as test F4 |
Action |
8 weeks |
Jackson |
Update code to SPC v3.1 |
Incorporate the improvements that Gaskell added to SPC during the Rosetta mission. Supports pole wobble more effectively |
Action |
16 weeks |
SPOC |
Max Slope |
Do a paremeter study of the impact of the MXSLP variable, currently used for 0.6 |
Action |
4 weeks |
Jackson |
OLA Albedo Integration |
Work out integration of albedo into OLA |
Action |
3 weeks |
Lockheed - Lorenz |
Pole and Omega on F4 |
Need to run the pole and omega using F4's final shape model. May need Gaskell to train |
Action |
2 weeks |
Palmer |
High |
||||
FDS Integration |
Develop the procedures and run an Approach/PreSurvey test that works on the transition to landmark navigation that contains multiple sets of data being passed |
High |
8 weeks |
FDS |
Image Quality |
Generate a shape model using low(er) quality images that contain PSF, blur, hot pixels and cosmic rays |
High |
8 weeks |
AltWG |
Asteroid wall |
Process Lockheed's asteroid wall |
High |
12 weeks |
Lockheed |
NFT-SPC Thread Test |
Generate NFT Features and use for Decent to TAG simulation |
High |
scope is uncertain |
Lockheed - Lorenz |
Enhanced Imaging |
Develop requirements and imaging plan to support. Develop high resolution DTM's based upon it |
High |
12 weeks |
SPOC |
Center of Figure / Center of Mass |
SPC can shift the system of coordinates. FDS needs to have the COF mapped to COM for navigation |
High |
14 weeks |
FDS |
Medium |
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Operations Test: Parallel processing and team |
Run Preliminary Survey and Detailed Survey portions of the mission using multiple people and multiple machines |
Medium |
8 weeks |
SPOC |
Update F2/F3 with Cross Correlation |
Recompute the RMS using manually process and a Normalized Cross Correlation |
Medium |
5 weeks |
Palmer |
Low |
||||
|
|
Low |
2 weeks |
Palmer |
Must be prioritized |
||||
Dynamics test |
Do an evaluation of SCOBJ and PTG with and without the use of dynamics |
|
8 weeks |
Palmer |
Uncertainty test |
See the effect of different amounts of uncertainty in the solution of SPC |
|
8 weeks |
Palmer |
Have starting model signif different than truth |
The existing Shape 4 is only 2 meters different than the Nolan model. Run a test where we greatly increase the deviation between starting and truth |
|
12 weeks |
Jackman |
NavCam distortion |
Put in camera distortion for the source images and see how well SPC removes it. This is more needed for NavCam |
|
5 weeks |
Jackman |
Size vs. speed error |
Have a model that has a systematic error so that the size of the model is off. Then use Gaskell's speed correction analysis to identify and fix a size variation |
|
6 weeks |
Palmer |
Anybody want anything else?