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NASA NTRS · 20110011944

Self-Balancing, Optical-Center-Pivot, Fast-Steering Mirror

Abstract

A complete, self-contained fast-steering- mirror (FSM) mechanism is reported consisting of a housing, a mirror and mirror-mounting cell, three PZT (piezoelectric) actuators, and a counterbalance mass. Basically, it is a comparatively stiff, two-axis (tip-tilt), self-balanced FSM. The present invention requires only three (or three pairs for flight redundancy) actuators. If a PZT actuator degrades, the inherent balance remains, and compensation for degraded stroke is made by simply increasing the voltage to the PZT. Prior designs typically do not pivot at the mirror optical center, creating unacceptable beam shear.

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Moore, James D., Carson, Johnathan W.. 2011-04-01. Self-Balancing, Optical-Center-Pivot, Fast-Steering Mirror. https://ntrs.nasa.gov/citations/20110011944

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