A system comprising: a first reflective surface configured to be positioned on a wing of an aircraft , the first reflective surface 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 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 is configured to: receive the first laser beam reflected from the first reflective surface ; and sense the first laser beam at a first identifiable position on the first light beam locating sensor ; and a processor configured to: receive a first signal from the first light beam locating sensor , the first signal including the first identifiable position on the first light beam locating sensor ; 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 if there is a difference in the first comparison. a first reflective surface configured to be positioned on a wing of an aircraft , the first reflective surface 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 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 is configured to: receive the first laser beam reflected from the first reflective surface ; and sense the first laser beam at a first identifiable position on the first light beam locating sensor ; and receive the first laser beam reflected from the first reflective surface ; and sense the first laser beam at a first identifiable position on the first light beam locating sensor ; and a processor configured to: receive a first signal from the first light beam locating sensor , the first signal including the first identifiable position on the first light beam locating sensor ; 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 if there is a difference in the first comparison. receive a first signal from the first light beam locating sensor , the first signal including the first identifiable position on the first light beam locating sensor ; 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 if there is a difference in the first comparison. <EOS>