The robust control of a general servomechanism problem is applied in the case of electrohydraulic servo actuating primary flight controls. The servocompensator structure is proved to be close to the one designed for step signals. The stabilizing compensator is ensured by the way of a linear quadratic optimal procedure. An antiwindup compensation is added to deal with the adverse effects caused by control saturation. The proof is made involving the form of a feedback compensation matrix. Numerical simulations are presented to validate the proposed procedure.
Read full abstract