Control system for reconfigurable rotary wing aircraft

A control system for a rotary wing aircraft having a reconfigurable element. The control system includes a model predictive control module receiving operator commands, objectives and constraints; and a dynamic inversion module receiving an output of the model predictive control module, the dynamic i...

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Bibliographic Details
Main Authors Sahasrabudhe, Vineet, Geiger, Derek, Greenfield, Aaron L, Rigsby, James
Format Patent
LanguageEnglish
Published 17.07.2018
Subjects
CONTROLLING
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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Summary:A control system for a rotary wing aircraft having a reconfigurable element. The control system includes a model predictive control module receiving operator commands, objectives and constraints; and a dynamic inversion module receiving an output of the model predictive control module, the dynamic inversion module providing control commands to reconfigure the reconfigurable element of the rotary wing aircraft.
Bibliography:Application Number: US201213396769