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OARE flight maneuvers and calibration measurements on STS-58The Orbital Acceleration Research Experiment (OARE), which has flown on STS-40, STS-50, and STS-58, contains a three axis accelerometer with a single, nonpendulous, electrostatically suspended proofmass which can resolve accelerations to the nano-g level. The experiment also contains a full calibration station to permit in situ bias and scale factor calibration. This on-orbit calibration capability eliminates the large uncertainty of ground-based calibrations encountered with accelerometers flown in the past on the orbiter, thus providing absolute acceleration measurement accuracy heretofore unachievable. This is the first time accelerometer scale factor measurements have been performed on orbit. A detailed analysis of the calibration process is given along with results of the calibration factors from the on-orbit OARE flight measurements on STS-58. In addition, the analysis of OARE flight maneuver data used to validate the scale factor measurements in the sensor's most sensitive range is also presented. Estimates on calibration uncertainties are discussed. This provides bounds on the STS-58 absolute acceleration measurements for future applications.
Document ID
19940028418
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blanchard, Robert C.
(NASA Langley Research Center Hampton, VA, United States)
Nicholson, John Y.
(NASA Langley Research Center Hampton, VA, United States)
Ritter, James R.
(NASA Langley Research Center Hampton, VA, United States)
Larman, Kevin T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1994
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-TM-109093
NAS 1.15:109093
Accession Number
94N32924
Funding Number(s)
PROJECT: RTOP 237-02-02-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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