主权项 |
1. A method for determining an aerodynamic force associated with an airfoil, the method comprising:
determining, by an airfoil control device, a pressure differential between a first pressure location and a second pressure location on an airfoil; determining, by the airfoil control device, at least two of: a rotation speed of the airfoil, an ambient air pressure, an ambient air temperature, and a pitch angle of the airfoil; and determining, by the airfoil control device, an aerodynamic force associated with the airfoil based on the pressure differential, and the at least two of: the rotation speed of the airfoil, the ambient air pressure, the ambient air temperature, and the pitch angle of the airfoil. |