The paper discusses the ways and methods of integrating parametric and non-parametric reconfiguration methods of on-board systems of a supersonic passenger aircraft in one hybrid controller. To develop a hybrid controller, a circuit with switching of parametric and non-parametric controllers is used. The choice of method is based on the availability of parametric information about the control object, current disturbances and the required control quality.
A Method for Constructing a Hybrid Controller for Reconfiguration of On-Board Systems of a Supersonic Passenger Aircraft in the Event of Failures
Springer Aerospace Techn.
2023-04-11
7 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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