Abstract
Influences of jitter caused by disturbance sources located inside of a spacecraft on its mission feasibility tend to be an important issue. Solar Array Drive Mechanisms (SADMs) are typical disturbance sources, and the micro-vibration caused by them is estimated from test results using hardware without Solar Array Panets (SAPs). This study validates traditional assumption that the SAPs are not needed to estimate response of micro-vibration in the middle frequency range.
