Looking at basic logistics in engineering.
Missile tubes are not a problem for C&C loop. But PDLC's or Grasers? Lets look at the calibration required.
Lets assume the Sensors for detection the position of incoming missiles do not get modularized and MOVED(might not be true, could make more sense to incorporate these sensors directly into the PDLC mount.
So, these sensors are in a fixed known position. Under normal LAC non modular working environment, the PDLC/GRASER mounts are at known positions once the LAC comes up to temperature and the structure stops growing due to thermal expansion. Likewise the structural deflections due to maneuvering are also known due to TESTING. Therefore when the shot of the PDLC at an incoming missile, the sensors and the PDLC are aligned.
Lets look at the radial accuracy required. Start non moving object and non moving LAC. Easiest Scenario. Radial accuracy required on a 1m target at 100,000km for a PDLC is arctan of 1m/100,000,000m. Of course the SD PDLC's are 1m/200,000km and worse yet for the Grasers at 500,000km, but lets make our life easier and use powers of 10. Now due to basic geometry we know that the same error radial angle must be present at the PDLC mount as well. How long is the PDLC mount(modular)? Lets call it 1m. Therefore the the maximum allowable PDLC mount error is 0.000000001 over said 1m.
Or 1 nanometers. = 10 Angstroms.
10 angstroms, depending on the material used is ~approx~ 5-10 atoms thick.
In short the modules in question better not have a single spec of dust, scratch, hair, flake of skin, or fingerprint on the mating surface.
Irregardless of how you would manufacture such a device. Lets just assume one could actually build such a device. Of course a single degree celsius of thermal expansion will grown said PDLC far more than 10A...
How realistic is that on something that is being moved around multiple times and having maintenance done on it? Then add in slop in the mechanism that latches these face modules onto the front of the LAC.
Now, could you have an automatic calibration system that adjusts for this difference in position? Split diffraction laser inferometer for instance? In three dimensions? Might have to have such a system in place due to simple maneuvering stresses placed on the LAC already. Difference in the structural deflection between 1g maneuver and a 0g maneuver will warp the PDLC/Sensor alignment. Offhand I would say this is already highly likely if one believes one is going to actually hit anything with a PDLC. Such a system would have to be in place for the electro-mechanical adjustment for tracking the moving object and placement of the lens in question.
Of course at the alignment required here, a simple discharge of electro static/magnetic forces, say charging the PDLC to fire it...
is going to move the lattice structure of the material itself changing the reflective properties of the material in question throwing off the inferrometer and therefore its aiming accuracy...
Enjoy your engineering 101...
LAC bays in a combat environment would have to be cleaner than the cleanest clean room here on earth....... Yea... phttttttt....
Shhhhh, don't worry, grasers hitting at 500,000 or 1,000,000 km would "only" require 1 angstrom out of alignment or less than half of a single average atomic radii nucli......