Wang Xi, Zeng Qingfu. ROBUST H∞ OUTPUT FEEDBACK CONTROL OF STRUCTURED AND UNSTRUCTURED PARAMETER UNCERTAIN SYSTEM FOR AEROENGINE[J]. Journal of Aerospace Power, 1999, 14(3): 305-308.
Citation:
Wang Xi, Zeng Qingfu. ROBUST H∞ OUTPUT FEEDBACK CONTROL OF STRUCTURED AND UNSTRUCTURED PARAMETER UNCERTAIN SYSTEM FOR AEROENGINE[J]. Journal of Aerospace Power, 1999, 14(3): 305-308.
Wang Xi, Zeng Qingfu. ROBUST H∞ OUTPUT FEEDBACK CONTROL OF STRUCTURED AND UNSTRUCTURED PARAMETER UNCERTAIN SYSTEM FOR AEROENGINE[J]. Journal of Aerospace Power, 1999, 14(3): 305-308.
Citation:
Wang Xi, Zeng Qingfu. ROBUST H∞ OUTPUT FEEDBACK CONTROL OF STRUCTURED AND UNSTRUCTURED PARAMETER UNCERTAIN SYSTEM FOR AEROENGINE[J]. Journal of Aerospace Power, 1999, 14(3): 305-308.
The robust stability and robust performance of aeroengine mixed uncertain system are analyzed.By introducing structured singular value μ synthesis method,the robust H∞ output feedback control is investigated under mixed structured and unstructured parameter perturbations.Disturbance rejection and servo tracking performance with the designed controllers for aeroengine uncertainty systems are simulated on a nonlinear model of twin-spool turbojet engine.
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