NASA NTRS · 19720000052
Adaptive position control loop
Abstract
Design of attitude control system for a sounding rocket is established by using a control loop which incorporates a lead network to convert position output into a feedback signal that is approximately proportional to position, plus a constant times rate.
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Keltz, W. L.. 1972-01-01. Adaptive position control loop. https://ntrs.nasa.gov/citations/19720000052
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