FGS/FHST Combined Pointing Control Mode On-Orbit Test

Details FGS/FHST Combined Pointing Control Mode On-Orbit Test FGS/FHST Combined Pointing Control Mode On-Orbit Test

Dec 1997

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1997hst..prop.7968i&link_type=abstract

HST Proposal ID #7968

Other

Hst Proposal Id #7968

Scientific paper

The purpose of the FGS/FHST On-Orbit Test is to verify the ability of the FGS/FHST Combined Pointing Control Mode to achieve the accuracy required to support science observations. This test should demonstrate that the predicted roll error and corresponding pointing error is not exceeded by the vehicle under each of the identified observing scenarios. The on-orbit test will verify each of the following: 1. Ability of each FHST to control roll. 2. Ability to hand-off roll control from one FHST to another. 3. Ability to configure FHST control before and after FGS control. 4. Roll stability under gyro control in cases where FHST settling time was and was not achieved {and thus whether the integral term is not or is zeroed}. 5. Ability to perform small angle maneuvers, especially while under gyro control.

Affiliated with

Also associated with

No associations

Rating

FGS/FHST Combined Pointing Control Mode On-Orbit Test does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.

If you have personal experience with FGS/FHST Combined Pointing Control Mode On-Orbit Test, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and FGS/FHST Combined Pointing Control Mode On-Orbit Test will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFWR-SCP-O-896484