2015
DOI: 10.1088/0264-9381/32/22/224017
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Gravity Probe B orbit determination

Abstract: The Gravity Probe B (GP-B) satellite was equipped with a pair of redundant Global Positioning System (GPS) receivers used to provide navigation solutions for real-time and post-processed orbit determination (OD), as well as to establish the relation between vehicle time and coordinated universal time. The receivers performed better than the real-time position requirement of 100 m rms per axis. Post-processed solutions indicated an rms position error of 2.5 m and an rms velocity error of 2.2 mm s−1. Satellite l… Show more

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Cited by 4 publications
(6 citation statements)
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“…GPS receiver. Every 10 s a GPS receiver provided GPS time and the position and velocity of the Spacecraft for the exact orbit determination described in paper 17 [31].…”
Section: Science Datamentioning
confidence: 99%
“…GPS receiver. Every 10 s a GPS receiver provided GPS time and the position and velocity of the Spacecraft for the exact orbit determination described in paper 17 [31].…”
Section: Science Datamentioning
confidence: 99%
“…were used to calculate the instantaneous values of g Ω ⃗ and fd Ω ⃗ (in fact, the J 2 correction to the frame-dragging was negligible). These were computed for every orbit from the precise GPS orbit data [21] using each available valid data point. The averages found differed slightly from orbit to orbit due its small classical variation, so we Ω 〈 〉and ns Ω 〈 〉 were additionally averaged over all orbits, and relativistic drift rate predictions were determined from the result given by the formulas (11).…”
Section: ≡ ×mentioning
confidence: 99%
“…( ) μ⃗ being the misalignment vector (21). Here we used expression (27) for ψ , took ψ equal to μ according to equation (26), and introduced the torque coefficient ( ) ( ) taking into account that H l0 is real.…”
Section: C2 Pe Torques On the Spinning Rotor Inside Rolling Housing: ...mentioning
confidence: 99%
“…The uncertainties in the predicted drift rates for the GP-B gyroscopes are dominated by the uncertainty in the S/C orbit. S/C position and velocity were determined using on-board GPS [24]. The data were fit in 30 h-long batches.…”
Section: 43mentioning
confidence: 99%
“…Figure24. Relativistic drift rate estimates for gyroscope 3 using only data from individual segments (colored ellipses) and using all segments (black ellipse).…”
mentioning
confidence: 99%