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.
Adaptive position control loop
1972-01-01
Miscellaneous
No indication
English
Dynamic Matrix Control for ACU Position Loop
Springer Verlag | 2014
|Dynamic Matrix Control for ACU Position Loop
British Library Conference Proceedings | 2015
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|Adaptive Inner-Loop Rover Control
NTRS | 2006
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