Derivative-Free Output Feedback Adaptive Control of an Aeroelastic Generic Transport Model
نویسندگان
چکیده
This paper illustrates an application of derivative-free, output feedback adaptive control on an aeroelastic model of longitudinal dynamics for a generic transport model. The controller uses a state observer as a reference model, and has a derivative-free delayed weight update law. Since it does not assume the existence of constant ideal weights, it is particulary well suited for adaptation to sudden changes in system dynamics, such as might be due to reconfiguration, deployment of a payload, docking, structural damage, or to difficult to model external disturbances. In addition, it is applicable to output feedback adaptive control design for non-minimum phase plants.
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