A control system (100) for a rotary wing aircraft having a reconfigurable element. The control system includes a model predictive control module (110)receiving operator commands (102), objectives (112) and constraints (106); and a dynamic inversion module (116) receiving an output (114) of the model predictive control module (110), the dynamic inversion module (116) providing control commands to reconfigure the reconfigurable element (118) of the rotary wing aircraft.
Control system for reconfigurable rotary wing aircraft
Steuersystem für rekonfigurierbaren Drehflügler
Système de commande pour aéronef à voilure tournante reconfigurable
2019-06-12
Patent
Electronic Resource
English
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