gateWidth is the instantaneous FoV of the seeker without stuff like the sidewinders expanded acquisition mode, which is more or less a rapid area search more than a widened FoV. Other ordnance has the ability to increase or decrease FoV, some just has a very small FoV to begin with.
Ultimately the concept is simple, a smaller FoV and discriminatory wavelength detection to focus on that closer to airframe emissions.
I have been trying to find one that specifies the PL-8B’s capabilities. I may try to get into contact with a technical university soon to ask if they have any papers that aren’t available on the internet.
There’s a paper called Simulation and Analysis of 4-unit Infrared Guiding-head’s Anti-jamming Principle. One of the author came from the Eighth Institute of Airforce so it’s reliable.
Spoiler
Section 2.1 of the paper outlines the 4-unit infrared guiding-head’s anti-jamming principle. It have both seeker shutoff (main) and gatewidth (about 1°)
Why are we even arguing for suspension IRCCM? That’s not what it uses IRL. It should be for the time being a copy-paste TY-90 seeker until they model the more advanced features of IRCCM. If they modeled it accurately, it would effectively be gatewidth with it’s own algorithm for rejecting flares (not suspension, suspension is the weakest algorithm you can have for this type of IRCCM). If they really wanted to model it accurately, they would have to have the algorithm simulate what the multi-element array is seeing on the gain/return and making decisions based off that data.
That would make it incredibly strong and almost impossible to flare. There’s a reason both this missile and the AAM-3 don’t have their IRL seeker capabilities. The game isn’t ready for it, at least not until defensive countermeasures, EW, and jamming are properly implemented.