Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1767265 | Advances in Space Research | 2007 | 10 Pages |
Abstract
The Gravity Probe B (GP-B) Relativity Mission is a fundamental physics experiment to test Einstein's theory of General Relativity based on observations of spinning gyroscopes onboard a satellite in a near-polar, near-circular orbit at an altitude of about 640Â km around the Earth. The GP-B mission was designed to test two predictions of Einstein's theory, the geodetic effect and the frame-dragging effect, to an accuracy better than 5Â ÃÂ 10â4Â arcsec/yr. Drag-free control technology is implemented in the GP-B translation control system to minimize support forces and support induced torques on the gyroscopes. A Global Positioning System (GPS) receiver onboard the GP-B satellite provides real-time position, velocity and timing data. The GP-B orbit is determined on the ground based on the 3-axis GPS position data and verified independently with ground-based laser ranging measurements. This paper describes the design and implementation of the drag-free translation control and orbit determination system of the GP-B satellite. The on-orbit performance of the drag-free translation control system satisfies the requirements of the GP-B science experiment. The residual accelerations from the gyroscope control efforts are less than 4Â ÃÂ 10â11Â m/s2 (along the satellite roll axis) and less than 2Â ÃÂ 10â10Â m/s2 (transverse to the satellite roll axis) between 0.01Â mHz and 10Â mHz in inertial space. The non-gravitational acceleration along the satellite roll axis, including a nearly constant component (which is kept below 1Â ÃÂ 10â7Â m/s2) and a sinusoidal component (whose amplitude varies from about 5Â ÃÂ 10â7Â m/s2 to less than 1Â ÃÂ 10â8Â m/s2), causes the gyroscope spin axis to drift less than 9Â ÃÂ 10â5Â arcsec/yr. The orbit determination system is found to provide overlapping orbit solution segments having RMS (root mean square) position and velocity errors of a few meters and a few mm/s, well within the RMS mission requirements of 25Â m and 7.5Â cm/s.
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
J. Li, W.J. Bencze, D.B. DeBra, G. Hanuschak, T. Holmes, G.M. Keiser, J. Mester, P. Shestople, H. Small,