It’s funny because air gapping the INS units from each other and then flagging a disagreement is basically how the old Delco Carousel INS system worked - the ones you’d see on the Concorde, 747 classic, etc:
View attachment 75053
Rectangular display unit, with key pad and a dummy display, to be used to enter waypoints and other navigational information for a long-range commercial airliner.This is the display and keyboard, manufactured by the Delco Division of General Motors, for an Inertial Navigation Sys
airandspace.si.edu
I’ve never used them but I’ve watched enough old aviation videos to know that the Orange remote button would link them together for INIT POS, then you’d deselect it and the three INSes would float separately for the duration of the flight (which included long international flights with ocean crossings, etc). I believe there was a comparative logic built it that was smart enough where if one unit drifted enough relative to the other two it would alert and then the remaining two would vote that one off the island.
Any retired JC members get to use these things early in their career?
It’s kind of hilarious that Concordes were crossing the Atlantic at twice the speed of sound with these things in the 70s and now here we are in 2023 lamenting how we’ll ever be able to figure out how an INS/GPS disagree in our subsonic airliners.
The answer is simple - it was arrogant for avionics engineers to consider GPS as an infallible truth source. It’s not. Spoofing works by the gradual introduction of error and al
lowing the systems to update the INS position multiple times… it shouldn’t work that way. Original calculated INS position should continue to be tracked in memory for the duration of the flight and air gapped from each other, just as it was with the old Delco units. Rather than a truth source, GPS becomes a 4th “potential” position source weighted against the others. And since laser ring gyros are pretty darn accurate one can predict how much their maximum allowable drift should be over the duration of your flight - then your computer could cross-check that against GPS. Has the GPS position drifted more than the allowable INS drift? Then you are being spoofed, and your GPS data is bogus - vote kick it and revert to averaged INS position using the pre-corrected values stored in memory.
We definitely have the tech to do this, the current systems are just unequally weighing the inputs. Add in a 5th ground based nav input with DME/DME and we really have no excuse.