Quadratically stable H∞ robust controller for the integrated flight/propulsion control system
Abstract：Being built up, the mathematics model of the plant is always influenced by the parameters uncer-tainties. Whatever control theory used for the integrated flight/propulsion control, it is necessary to besure that the flight/propulsion closed loop control system has the strong robust stability. This paper ap-plies the H∞ theory to the flight/propulsion control system. The following questions can be covered inthis paper:the quadratically stability concept mentioned in the flight/propulsion control; Hoo controller forflight/propulsion control designed; digitally simulation of the flight/propulsion control closed loop sys-tem; the satisfied conclusion to prove the system meets the robust requirements of the flight/propulsion
control system.
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Publication Date：2001-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：4( 19-22 )