NASA NTRS · 19920000131
Thrust-Vector-Control System
Abstract
Control gains computed via matrix Riccati equation. Software-based system controlling aim of gimbaled rocket motor on spacecraft adaptive and optimal in sense it adjusts control gains in response to feedback, according to optimizing algorithm based on cost function. Underlying control concept also applicable, with modifications, to thrust-vector control on vertical-takeoff-and-landing airplanes, control of orientations of scientific instruments, and robotic control systems.
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Murray, Jonathan. 1992-02-01. Thrust-Vector-Control System. https://ntrs.nasa.gov/citations/19920000131
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