The purpose of this project is to develop an instrument jitter correction system
In this study, we are only addressing the bore-sight changes due to internal instrument motions (tip/tilt). The roll alignment jitter component will need to be monitored and controlled by the S/C platform.More »
This begins to correct spacecraft and instrument jitter allowing the COEDI science instrument located in geostationary orbit to meet pointing stability requirements. Other concepts might also be able to use this technique.More »
|Organizations Performing Work||Role||Type||Location|
|Goddard Space Flight Center (GSFC)||Lead Organization||NASA Center||Greenbelt, MD|
|SGT, Inc.||Supporting Organization||Industry|
A final report document may be available for this project. If you would like to request it, please contact us.