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Robust tracking control of an aircraft with critical actuator jam failures

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Funding information Army Research Laboratory, Grant/Award Number: W911NF-15-2-0042 Abstract In this paper, we present a new single fixed controller approach based on the multivariable H2 control/regulator theory with internal model… Click to show full abstract

Funding information Army Research Laboratory, Grant/Award Number: W911NF-15-2-0042 Abstract In this paper, we present a new single fixed controller approach based on the multivariable H2 control/regulator theory with internal model principle to solve a challenging control problem arising from an on-flight critical elevator jam at random positions that otherwise would need switching numerous controllers or online adaptive redesign approaches.

Keywords: robust tracking; jam; control; aircraft critical; tracking control; control aircraft

Journal Title: Asian Journal of Control
Year Published: 2019

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