NASA NTRS · 19730000466
Solid-state controller
Abstract
Attitude controllers are used to guide roll, pitch, and yaw of vehicle in flight. Controllers enclose multitude of switches, gears, cams, and other hardware needed to transmit pilot's commands to attitude control systems. New design, using magnetic coupled transducers, eliminates many mechanical parts, improving reliability and reducing maintenance.
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Bailey, C. L.. 1974-03-01. Solid-state controller. https://ntrs.nasa.gov/citations/19730000466
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