NASA NTRS · 19840047803
Analytic solutions for dual-spin spacecraft during platform motion
Abstract
This paper presents analytic solutions to the dynamic equations of dual-spinners during platform slews. The rotor is assumed to be an axisymmetric balanced rigid body. The platform is an asymmetric rigid body with small static and dynamic imbalances. The solutions given in this paper extend a previous theory which provided an approximate solution only in the steady state.
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Hayati, S., Hamidi, M.. 1984-01-01. Analytic solutions for dual-spin spacecraft during platform motion. https://ntrs.nasa.gov/citations/19840047803
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