Title :
On approximating the step response of a third-order linear system by a second-order linear system
Author_Institution :
Hughes Aircraft Company, Fullerton, CA, USA
fDate :
12/1/1968 12:00:00 AM
Abstract :
A third-order linear system possessing type A step response closely approximates the step response of an equivalent second-order linear system. This correspondence presents curves of the equivalent second-order system damping factor and undamped natural frequency within the type A region.
Keywords :
Linear systems; Aircraft; Automatic control; Control systems; Damping; Feedback; Frequency; Linear systems; State-space methods; Transfer functions;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1968.1099055
