The work is organized as follows. A finite element model of the uncontrolled, non-actuated structure is used to obtain the plant model for actuator torque and displacement control. After having characterized and simulated pure rotary actuator behavior over the structure, selected target wing shapes corresponding to rigid trailing edge rotations are achieved through both open-loop and closed-loop control logics. |
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CITATIONS
Cited by 14 scholarly publications.
Actuators
Control systems
Aerodynamics
Control systems design
Adaptive control
Servomechanisms
Sensors