A system comprising: a first reflective surface (88, 208) configured to be positioned on a wing of an aircraft, the first reflective surface (88, 208) being associated with a first position to be located on the wing; a first laser configured to be secured to a fuselage of the aircraft and positioned to emit a first laser beam onto the first reflective surface; a first transparent panel configured to be positioned spaced apart from and in an overlying relationship to the first laser, wherein a surface of the first transparent panel is configured to conform to a surface of the fuselage; a first light beam locating sensor (52, 206) configured to be secured to the fuselage and associated with the first position to be located on the wing, wherein the first light beam locating sensor (52, 206) is configured to: receive the first laser beam reflected from the first reflective surface (88, 208); and sense the first laser beam at a first identifiable position on the first light beam locating sensor (52, 206); and a processor configured to: receive a first signal from the first light beam locating sensor (52, 206), the first signal including the first identifiable position on the first light beam locating sensor (52, 206); determine a location of the first position to be located on the wing; perform a first comparison of the location of the first position to be located on the wing to a predetermined analyzed location of the first position to be located on the wing; and send a first instruction to control moving of a movable control surface (244, 246, 254) if there is a difference in the first comparison. a first reflective surface (88, 208) configured to be positioned on a wing of an aircraft, the first reflective surface (88, 208) being associated with a first position to be located on the wing; a first laser configured to be secured to a fuselage of the aircraft and positioned to emit a first laser beam onto the first reflective surface; a first transparent panel configured to be positioned spaced apart from and in an overlying relationship to the first laser, wherein a surface of the first transparent panel is configured to conform to a surface of the fuselage; a first light beam locating sensor (52, 206) configured to be secured to the fuselage and associated with the first position to be located on the wing, wherein the first light beam locating sensor (52, 206) is configured to: receive the first laser beam reflected from the first reflective surface (88, 208); and sense the first laser beam at a first identifiable position on the first light beam locating sensor (52, 206); and receive the first laser beam reflected from the first reflective surface (88, 208); and sense the first laser beam at a first identifiable position on the first light beam locating sensor (52, 206); and a processor configured to: receive a first signal from the first light beam locating sensor (52, 206), the first signal including the first identifiable position on the first light beam locating sensor (52, 206); determine a location of the first position to be located on the wing; perform a first comparison of the location of the first position to be located on the wing to a predetermined analyzed location of the first position to be located on the wing; and send a first instruction to control moving of a movable control surface (244, 246, 254) if there is a difference in the first comparison. receive a first signal from the first light beam locating sensor (52, 206), the first signal including the first identifiable position on the first light beam locating sensor (52, 206); determine a location of the first position to be located on the wing; perform a first comparison of the location of the first position to be located on the wing to a predetermined analyzed location of the first position to be located on the wing; and send a first instruction to control moving of a movable control surface (244, 246, 254) if there is a difference in the first comparison.