Rapid Initial Detumbling Strategy for Micro/Nanosatellite with Pitch Bias Momentum System
Abstract:When a satellite separates from the launch vehicle, an initial high angular rate or a tip-off rate is generated. B-dot logic is generally used for controlling the initial tip-off rate. However, it has the disadvantage of taking a relatively long time to control the initial tip-off rate. To solve this problem, this paper suggests a new detumbling control method to be able to adapt to micro/nanosatellite with the pitch bias momentum system.Proposed detumbling method was able to control the angular rate within 20… Show more
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