TY  - JOUR
AB  - A method of designing the controller to solve the robust servomechanism problem is applied in the case of an electrohydraulic servo actuating primary flight control. This method is based on the well‐known solution consisting of two separate devices: a servocompensator, in fact an internal model of the exogenous dynamics, including the reference commands and disturbance signals; and a stabilizing compensator. The proof is made involving the servocompensator structure which is close to the one designed for step signals. The stabilizing compensator is assured by way of a linear quadratic optimal procedure. An antiwindup compensation is added to deal with the adverse effects caused by actuator saturation.
VL  - 70
IS  - 4
SN  - 0002-2667
DO  - 10.1108/00022669810225287
UR  - https://doi.org/10.1108/00022669810225287
AU  - Ursu I.
AU  - Tecuceanu G.
AU  - Ursu F.
AU  - Sireteanu T.
AU  - Vladimirescu M.
PY  - 1998
Y1  - 1998/01/01
TI  - From robust control to antiwindup compensation of electrohydraulic servo actuators
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 259
EP  - 264
Y2  - 2024/04/25
ER  -