Each Skate is divided into two systems that each have their own control system.  The most critical part of the system is aligning and mating the mid and aft fuselage sections which arrive at Marietta from Lockheed Martin in Fort Worth and Boeing in Everett, respectively.  The wings cross this joint and it thus has a very high tolerance.  This is a fully automated machine vision/servo actuated system called the Mid Aft Mate Alignment System (MAMAS).  The MAMAS system rides atop the manually driven platforms that are used to drive freely on the aisleways from the end of the production line back to the beginning, or in a highly constrained way to drive from station to station on the assembly line with the fuselage at various stages of partial mate.  This system is called the Progressive Assembly Platform Automation System (PAPAS).

Jacks at each end of the line allow the user to transition the Skate from “freewheeling” to being forced into following a straight line (within 0.005” across 278 feet of length).  The PAPAS allow the Skates to move between stations with only part of the interference-fit holes drilled, without concern about losing position.  The PAPAS moves the fuselage sections together so they are close enough for the MAMAS to operate.

The Skates have built-in scissors lifts, under-belly lights with polycarbonate covers, 110V and 208V/3 phase electrical power, and pneumatic power with two hose diameters all built in throughout each Skate. When on its casters, the PAPAS can turn on its own center, or any radius desired. The PAPAS system is battery powered with a charging station built in at one of the work cells.  The system was designed to make 5 laps around the assembly line on a single charge.

Creating the mate joint with very high precision is critical.  An alignment of the large fuselage sections is required first, and then the mid and aft are slid together as a stovepipe fitting.  The multi-dimensional jacks at the hard-points of each fuselage section support the aircraft sections and move them as needed in 6 degrees of freedom.

The machine vision system can measure the alignment of the mid and aft sections with respect to a tooling fixture that represents “a perfect wing”. If all the fuselage lugs are aligned with their wing lugs, then the fuselage sections are attached together while everything is held rigid for several weeks and station-to-station moves, the wings will attach with no reaming or boring.  The entire F-22 production run was made without a single wing requiring any special action to bolt on.  Any right-hand wing fits on the right side of any F-22 fuselage, as do the lefts.

A machine vision camera called a “vision pin” is mounted inside a precision housing and a calibration method was devised to determine the precise center of image sensor.  On an opposite facing clevis, a precision bored face of a “light pin” is exposed to the camera.  These two items essentially create a virtual alignment pin that is made of a light beam.  It is extremely accurate and as it is made exclusively of photons, it never gets stuck while trying to make a complex alignment and mate.

When the wing lug is between the two halves of the “pin”, the camera can measure the position of the wing lug relative to the light pin.  An algorithm developed by Delta Sigma then computes how to move 7 axes such that the fore and aft part of each fuselage module is adjusted in six degrees of freedom concurrently to arrive at the proper alignment.  This alignment occurs before the sections are mated.  The camera’s traverse axes (water and butt) are measured by the camera to an accuracy of 0.0001 inch and the in-line axis (station) has an accuracy of 0.001 inch.  The user can view any of the eight Vision Pin views, but typically does not need to do so. 

It is essential to note the system is not a simple closed loop tracking system with each vision pin independently attempting to achieve an independent goal.  Three-dimensional measurements are being made in 4 places on each fuselage module.  Three-dimensional motion is being induced in 4 other places on each fuselage module.  The motion induced from any position affects the measurements in all axes at all positions.  Conversely, to achieve a three-dimensional alignment at any one measurement position, requires movement at all the hard-point positions.  The system works because the calculations to induce precisely the right motion to solve for 22 measurements using 7 axes of control on each module at each position determines how much and in what direction to move each motor before any movement take place.

The user screen allows the user to quickly see and understand the state of alignment in a glance.  There are four stations where Vision Pins are located, in each case – one left side and one right side.  Each circle represents a station and the colored “balls” represent the two sides.  The green balls in the alignment circles represent the average of the misalignments between the two sides.  On the lower left of the screen are status indicators of the Vision Pins and each of the servo axes.  If one is red, the system will not operate and clicking the red indicator will inform the operator the details of the fault.

When the left and right balls are within the outer circle, the MAMAS system is close enough to make accurate measurements.  Selecting “RUN” causes the alignment.  When the balls are within the inner circle, the water and butt alignment is within tolerance.  The station alignment is shown on the bar below the circles.

Vision System Design

https://www.vision-systems.com/home/article/16737418/visionguided-system-speeds-fa22-assembly

EDN

https://www.edn.com/taking-flight/