NASA NTRS · 19740055059
Engineering parameter determination from the radio astronomy explorer /RAE I/ satellite attitude data
Abstract
An RAE-I satellite description is given, taking into account a dynamics experiment and the attitude sensing system. A computer program for analyzing flexible spacecraft attitude motions is considered, giving attention to the geometry of rod deformation. The characteristics of observed attitude data are discussed along with an analysis of the main boom root angle, the bending rigidity, and the damper plane angle.
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Lawlor, E. A., Davis, R. M., Blanchard, D. L.. 1974-08-01. Engineering parameter determination from the radio astronomy explorer /RAE I/ satellite attitude data. https://ntrs.nasa.gov/citations/19740055059
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