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Effect of attitude control thruster induced structural vibrations on sensed accelerations of a space vehicle. [For making corrections for determining earth's gravity field from orbiting space vehicle]
Author(s) -
T.D. Butler
Publication year - 1977
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/7208562
Subject(s) - vibration , accelerometer , nonlinear system , physics , acceleration , excitation , equations of motion , control theory (sociology) , normal mode , space vehicle , acoustics , classical mechanics , computer science , astronomy , artificial intelligence , control (management) , quantum mechanics

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