NASA NTRS · 19990071658
Performance Evaluation Gravity Probe B Design
Abstract
This final report documents the work done to develop a 6 degree-of-freedom simulation of the Lockheed Martin Gravity Probe B (GPB) Spacecraft. This simulation includes the effects of vehicle flexibility and propellant slosh. The simulation was used to investigate the control performance of the spacecraft when subjected to realistic on orbit disturbances.
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Francis, Ronnie, Wells, Eugene M.. 1996-04-05. Performance Evaluation Gravity Probe B Design. https://ntrs.nasa.gov/citations/19990071658
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