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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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
17.07.2018
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Subjects | |
Online Access | Get full text |
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