Session L1: Poster Session II
2:00 PM–2:00 PM, Sunday, April 15, 2007
Hyatt Regency Jacksonville Riverfront Room: Terrace Pavilion, 2:00pm - 5:00pm
Sponsoring Unit:
APS
Abstract ID: BAPS.2007.APR.L1.25
Abstract: L1.00025 : Gravity Probe B Gyroscope Electrostatic Suspension System (GSS)
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Abstract 
Authors:
William Bencze
(Stanford University)
David Hipkins
(Stanford University)
Tom Holmes
(Stanford University)
Saps Buchman
(Stanford University)
Robert Brumley
(Boeing Company)
Presented here is a hybrid digital/analog electrostatic suspension control system for the Gravity Probe B Relativity Mission's science gyroscopes. The chief challenge for this system is to operate over 8 orders of force magnitude while minimizing classical torques on the gyroscope. A novel, adaptive LQE digital control algorithm was developed to meet the high dynamic range requirements for rotor suspension, while minimizing suspension-induced torques. A set of three backup, all-analog proportional-derivative (PD) controllers were provided to maintain rotor centering in the event of computer faults during all phases of the mission. The capacitive position sensing system measured rotor position to a noise floor of 0.15 nm/$\surd $Hz in the science band (5 - 30 mHz). In addition, this system also applied controlled torques to perform a post spin-up alignment of the gyroscope spin axes to within 10 arc-sec of a desired orientation, and measured the rotor charge to the 2 pC (2 mV) level. The GSS contributed to drag-free operation of the space vehicle by using one of the gyroscopes as an isolated, inertial proof mass and was able to resolve accelerations to the 10$^{-12 }$g level. On-orbit performance of this system will be discussed in detail.
To cite this abstract, use the following reference: http://meetings.aps.org/link/BAPS.2007.APR.L1.25