Unbiased acceleration measurements with an electrostatic accelerometer on a rotating platform
arXiv:1105.4979 · doi:10.1016/j.asr.2012.08.012
Abstract
The Gravity Advanced Package is an instrument composed of an electrostatic accelerometer called MicroSTAR and a rotating platform called Bias Rejection System. It aims at measuring with no bias the non-gravitational acceleration of a spacecraft. It is envisioned to be embarked on an interplanetary spacecraft as a tool to test the laws of gravitation. MicroSTAR is based on Onera's experience and inherits in orbit technology. The addition of the rotating platform is a technological upgrade which allows using an electrostatic accelerometer to make measurements at low frequencies with no bias. To do so, the Bias Rejection System rotates MicroSTAR such that the signal of interest is separated from the bias of the instrument in the frequency domain. Making these unbiased low-frequency measurements requires post-processing the data. The signal processing technique developed for this purpose is the focus of this article. It allows giving the conditions under which the bias is completely removed from the signal of interest. And the precision of the unbiased measurements can be fully characterized: given the characteristics of the subsystems, it is possible to reach a precision of 1 pm s on the non-gravitational acceleration for an integration time of 3 h.
14 pages, 6 figures, new formatting, minor amendments
References in corpus (14)
- The Confrontation between General Relativity and Experiment
- Dark Energy and the Accelerating Universe
- Support for the thermal origin of the Pioneer anomaly
- Quantum Physics Exploring Gravity in the Outer Solar System: The Sagas Project
- High precision thermal modeling of complex systems with application to the flyby and Pioneer anomaly
- Thermal gradient-induced forces on geodetic reference masses for LISA
- Support for temporally varying behavior of the Pioneer anomaly from the extended Pioneer 10 and 11 Doppler data sets
- Odyssey: a Solar System Mission
- OSS (Outer Solar System): A fundamental and planetary physics mission to Neptune, Triton and the Kuiper Belt
- Electrostatic accelerometer with bias rejection for Gravitation and Solar System physics
- Pioneer 10 Doppler data analysis: disentangling periodic and secular anomalies
- A mission to test the Pioneer anomaly: estimating the main systematic effects
- A Mission to Explore the Pioneer Anomaly
- Measuring the absolute non-gravitational acceleration of a spacecraft: goals, devices, methods, performances
Cited by in corpus (5)
- OSS (Outer Solar System): A fundamental and planetary physics mission to Neptune, Triton and the Kuiper Belt
- The local dark sector. Probing gravitation's low-acceleration frontier and dark matter in the Solar System neighborhood
- Experimental demonstration of bias rejection from electrostatic accelerometer measurements
- Measuring the absolute non-gravitational acceleration of a spacecraft: goals, devices, methods, performances
- Electrostatic accelerometer with bias rejection for deep space gravitation tests