Title :
Servo actuator peak power output for step input signals
Author_Institution :
Martin Co., Orlando, FL, USA
fDate :
4/1/1964 12:00:00 AM
Keywords :
Actuators; Servosystems; Aerospace control; Control systems; Damping; Equations; Frequency; Friction; Hydraulic actuators; Limit-cycles; Missiles; Servomechanisms;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1964.1105667
