f2dd4bb501b04e8d706c711e6dde5a954be75dce,trunk/SUAVE/Components/Energy/Networks/Serial_Hybrid_Ducted_Fan.py,Serial_Hybrid_Ducted_Fan,evaluate_thrust,#Serial_Hybrid_Ducted_Fan#,67

Before Change

        payload.power()

        // Calculate the esc input current
        esc.inputs.currentout =  np.transpose(motor_power/np.transpose(esc.outputs.voltageout))
        
        // Run the esc
        esc.currentin(conditions)

After Change

        // Calculate ducted fan power
        results             = propulsor.evaluate_thrust(state)
        propulsive_power    = np.reshape(results.power, (-1,1))
        motor_power         = propulsive_power/self.motor_efficiency 
      
        // Set the esc input voltage
        esc.inputs.voltagein = self.voltage

Instances