Modelagem de Um Amortecedor de Nutacao Para Satelites Estabilizados Por Rotacao (Modeling of a Nutation Damper for Satellite Stabilization Through Rotation)

摘要

The modeling is presented of a partially filled off set ring nutation damper. The different actuation modes of this equipment as well as the experimental tests for its performance evaluation were considered. The theoretical basis is supplied to the design of a nutation damper for the first MECB's satellite.