DocumentCode :
341253
Title :
Comparison tools for assessing the microgravity environment of orbital missions, carriers and conditions
Author :
DeLombard, Richard ; Hrovat, Kenneth ; McPerson, K.M.
Author_Institution :
NASA Lewis Res. Center, Cleveland, OH, USA
Volume :
2
fYear :
1999
fDate :
1999
Firstpage :
929
Abstract :
The principal component spectral analysis and the quasi-steady three-dimensional histogram techniques provide the means to describe, on a single plot, the micro-gravity acceleration environment of a long period of time, such as a day, week, or month. This allows a straight forward comparison of the micro-gravity environment between micro-gravity increments on the International Space Station, locations within the International Space Station, and/or different operating conditions. Traditional data display methods (e.g. acceleration versus time), while adequate for shorter time periods, would utilize more plots for an extensive period of time, often making interpretation more difficult. These new techniques provide a single page representation of a large set of micro-gravity acceleration data. These techniques, in conjunction with other techniques, may be employed to derive useful information from acceleration data to characterize or compare the micro-gravity environment
Keywords :
principal component analysis; space research; space vehicles; zero gravity experiments; International Space Station; acceleration data; microgravity environment; orbital missions; principal component spectral analysis; quasi-steady three-dimensional histogram techniques; single page representation; Acceleration; Accelerometers; Displays; Extraterrestrial measurements; Frequency; Gravity; Instruments; NASA; Space stations; Spectral analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation and Measurement Technology Conference, 1999. IMTC/99. Proceedings of the 16th IEEE
Conference_Location :
Venice
ISSN :
1091-5281
Print_ISBN :
0-7803-5276-9
Type :
conf
DOI :
10.1109/IMTC.1999.776999
Filename :
776999
Link To Document :
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