Abstract: A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.

Abstract: Safety architecture for an automated work cell provides a barrier separating a work cell area from an operator or personnel area. The safety architecture enables personnel to conduct routine interactions with nonfunctioning motion platforms or positioning machines located in the work cell area through openings in the barrier separating the personnel area from the work cell area while other motion platforms or positioning machines in the work cell area continues to function.

Abstract: Compliant end effectors, robots that include compliant end effectors, and methods of utilizing the same. The robots include a robotic arm and the compliant end effector. The compliant end effector includes a base, a jaw fixedly coupled to the base, a part-engaging surface, and a pivot structure. The pivot structure extends between the part-engaging surface and the jaw and is configured to permit limited rotation of the part-engaging surface relative to the jaw about a single pivot axis. The methods include locating an apparatus with a vision system of the robot, locating a part with the vision system, gripping the part with the compliant end effector, positioning the part relative to the apparatus, and operatively attaching the part to the apparatus. The positioning includes deliberately contacting a toe end of a flange of the part with the apparatus prior to contacting a heel end of the flange with the apparatus.

Abstract: A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.

Abstract: A method and apparatus for maintaining a selected configuration for a structure. Metrology data for a support system is received while the support system holds the structure. A determination is made as to whether a current configuration of the structure is within selected tolerances of the selected configuration for the structure based on the metrology data. The support system is moved to move the structure held by the support system into the selected configuration in response to a determination that the current configuration of the structure is not within the selected tolerances of the selected configuration for the structure.

Abstract: A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.

Abstract: A method and apparatus for maintaining a selected configuration for a structure. Metrology data for a support system is received while the support system holds the structure. A determination is made as to whether a current configuration of the structure is within selected tolerances of the selected configuration for the structure based on the metrology data. The support system is moved to move the structure held by the support system into the selected configuration in response to a determination that the current configuration of the structure is not within the selected tolerances of the selected configuration for the structure.

Abstract: Compliant end effectors, robots that include compliant end effectors, and methods of utilizing the same. The robots include a robotic arm and the compliant end effector. The compliant end effector includes a base, a jaw fixedly coupled to the base, a part-engaging surface, and a pivot structure. The pivot structure extends between the part-engaging surface and the jaw and is configured to permit limited rotation of the part-engaging surface relative to the jaw about a single pivot axis. The methods include locating an apparatus with a vision system of the robot, locating a part with the vision system, gripping the part with the compliant end effector, positioning the part relative to the apparatus, and operatively attaching the part to the apparatus. The positioning includes deliberately contacting a toe end of a flange of the part with the apparatus prior to contacting a heel end of the flange with the apparatus.

Abstract: A method and apparatus for maintaining a selected configuration for a structure during a manufacturing process for forming a product using the structure. Metrology data for a support system is received. The support system holds the structure during the manufacturing process. A determination is made as to whether a current configuration of the structure is within selected tolerances of the selected configuration for the structure based on the metrology data. The support system is reconfigured to move the structure into the selected configuration in response to a determination that the current configuration of the structure is not within the selected tolerances of the selected configuration for the structure.

Abstract: Compliant end effectors, robots that include compliant end effectors, and methods of utilizing the same. The robots include a robotic arm and the compliant end effector. The compliant end effector includes a base, a jaw fixedly coupled to the base, a part-engaging surface, and a pivot structure. The pivot structure extends between the part-engaging surface and the jaw and is configured to permit limited rotation of the part-engaging surface relative to the jaw about a single pivot axis. The methods include locating an apparatus with a vision system of the robot, locating a part with the vision system, gripping the part with the compliant end effector, positioning the part relative to the apparatus, and operatively attaching the part to the apparatus. The positioning includes deliberately contacting a toe end of a flange of the part with the apparatus prior to contacting a heel end of the flange with the apparatus.

Abstract: A method and apparatus for positioning one component relative to another component. First metrology data may be identified for a first component and second metrology data may be identified for a second component. First locations of first features may be identified on the first component using the first metrology data. Second locations of second features on the second component may be identified using the second metrology data. A transformation may be computed based on the first locations identified and the second locations identified for use in modifying a movement plan of a robotic system for positioning the second component relative to the first component.

Abstract: Compliant end effectors, robots that include compliant end effectors, and methods of utilizing the same. The robots include a robotic arm and the compliant end effector. The compliant end effector includes a base, a jaw fixedly coupled to the base, a part-engaging surface, and a pivot structure. The pivot structure extends between the part-engaging surface and the jaw and is configured to permit limited rotation of the part-engaging surface relative to the jaw about a single pivot axis. The methods include locating an apparatus with a vision system of the robot, locating a part with the vision system, gripping the part with the compliant end effector, positioning the part relative to the apparatus, and operatively attaching the part to the apparatus. The positioning includes deliberately contacting a toe end of a flange of the part with the apparatus prior to contacting a heel end of the flange with the apparatus.

Abstract: A method and apparatus for performing an operation on a surface of a structure. An assembly system may comprise a motion platform and a mobile platform. The motion platform may be configured to be positioned below the surface of the structure to perform the operation on the surface. The mobile platform may be configured to carry the motion platform across a floor of a manufacturing environment from a first location to a second location.

Abstract: A method and apparatus for performing an operation on a structure. In one illustrative embodiment, an apparatus comprises a tool system and a movement system. The tool system is configured to perform an operation at a location on a structure. The movement system is configured to move the tool system along an elongate frame on the structure to the location.

Abstract: A method and apparatus for positioning one component relative to another component. First metrology data may be identified for a first component and second metrology data may be identified for a second component. First locations of first features may be identified on the first component using the first metrology data. Second locations of second features on the second component may be identified using the second metrology data. A transformation may be computed based on the first locations identified and the second locations identified for use in modifying a movement plan of a robotic system for positioning the second component relative to the first component.

Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: A method and apparatus for maintaining a selected configuration for a structure during a manufacturing process for forming a product using the structure. Metrology data for a support system is received. The support system holds the structure during the manufacturing process. A determination is made as to whether a current configuration of the structure is within selected tolerances of the selected configuration for the structure based on the metrology data. The support system is reconfigured to move the structure into the selected configuration in response to a determination that the current configuration of the structure is not within the selected tolerances of the selected configuration for the structure.

Abstract: A method and apparatus for performing an operation on a surface of a structure. An assembly system may comprise a motion platform and a mobile platform. The motion platform may be configured to be positioned below the surface of the structure to perform the operation on the surface. The mobile platform may be configured to carry the motion platform across a floor of a manufacturing environment from a first location to a second location.

Abstract: A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.