Abstract
Due to the improvement of the complexity and diversity of modern aviation work, there are more requirements for the large altitude posture, the maneuverability and the accuracy of the tracking direction of flexible satellite for observing and tracking the ground. In this context, this paper discusses the large inclination maneuver attitude control theory and stability method of flexible satellites, and designs a shape memory alloy compression release device, which is expected to be used as a reference for relevant workers.
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