The Active Aeroelastic Wing will demonstrate technologies related to aeroservoelastic effects such as wing twist and load minimization. This paper presents a control design based on H-infinity synthesis that simultaneously considers the multiple objectives associated with handling qualities, actuator limitations, and loads. The controller is realized as a filter and gain set approximation to a state-space H-infinity controller. This approximation allows scheduling of the controller over a flight envelope.
Gain-Scheduled Approximations to H-Infinity Controllers for the F/A-18 Active Aeroelastic Wing
1999-01-01
Miscellaneous
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English
Gain-Scheduled Approximations to H-Infinity Controllers for the F/A-18 Active Aeroelastic Wing
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