Abstract: Apparatuses and methods are provided for a processing apparatus configured to authenticate an item based on at least one optical indicium associated with the item before processing the item. An interface may be configured to receive processing information from a machine readable element associated with an item to be processed. An image acquisition device may be configured to acquire image information relating to at least one optical indicium associated with an item. At least one processor may be configured to verify authentication of the item based upon the image information acquired by the image sensor unit. The processor may be further configured to receive processing information from the interface and to determine one or more instructions for processing the item based on the processing information. The apparatus may be further configured to processing the item in accordance with the instructions after the item has been verified as authentic.

Abstract: A method for providing a controllable side force to an air vehicle having a vertical stabilizer arrangement includes (a) selectively causing the vertical stabilizer arrangement to generate a first side force in a first side direction to provide the controllable side force, the first side force inducing a corresponding first yaw moment in a first yaw direction; and (b) selectively providing to the air vehicle a second yaw moment in a second yaw direction, the second yaw moment being induced by a force component of an auxiliary force applied to the air vehicle, the force component being in a force direction that is non-parallel with respect to the first side direction and the force component being spaced from a center of gravity of the air vehicle; wherein the second yaw direction is opposed to the first yaw direction. Also disclosed is a corresponding auxiliary yaw generating system.

Abstract: Apparatuses and methods are provided for a processing apparatus configured to authenticate an item based on at least one optical indicium associated with the item before processing the item. An interface may be configured to receive processing information from a machine readable element associated with an item to be processed. An image acquisition device may be configured to acquire image information relating to at least one optical indicium associated with an item. At least one processor may be configured to verify authentication of the item based upon the image information acquired by the image sensor unit. The processor may be further configured to receive processing information from the interface and to determine one or more instructions for processing the item based on the processing information. The apparatus may be further configured to processing the item in accordance with the instructions after the item has been verified as authentic.

Abstract: Methods and apparatuses for processing objects by RF energy are disclosed. In some embodiments the method may include grouping excitation setups into at least a first group corresponding to a first peak and a second group corresponding to a second peak. The method may further include applying RF energy such that an amount of RF energy absorbed at excitation setups of the first group is equal to an amount of RF energy absorbed at excitation setups of the second group. Apparatuses according to some embodiments may include a processor configured to carry out aspects of the method.

Abstract: A method for providing a controllable side force to an air vehicle having a vertical stabilizer arrangement includes (a) selectively causing the vertical stabilizer arrangement to generate a first side force in a first side direction to provide the controllable side force, the first side force inducing a corresponding first yaw moment in a first yaw direction; and (b) selectively providing to the air vehicle a second yaw moment in a second yaw direction, the second yaw moment being induced by a force component of an auxiliary force applied to the air vehicle, the force component being in a force direction that is non-parallel with respect to the first side direction and the force component being spaced from a center of gravity of the air vehicle; wherein the second yaw direction is opposed to the first yaw direction. Also disclosed is a corresponding auxiliary yaw generating system.