Earlier quoted context omitted.
It's not stable in a "crashes into the ground and kills everyone on board in spite of the best efforts of its pilots" manner. In exactly what manner is it not obvious this is not an acceptable design outcome?
You are confusing stability, which is a specific aerodynamic term, with two examples of catastrophic outcomes. Reread the original post I replied to, none of the first three sentences are true: unstable flight characteristics, instability is a hardware problem, software routine only exists to paper over the hardware problem. The problem results from an edge case or it would be happening a lot more often. That it's an…
You are right on target, but I do wish to point out the aerodynamics are still a problem, and a problem that has caused a great deal of grief in aviation history.
Take a trip down memory lane, and give the D.P. Davies Interview from the Royal Aeronautics Society a listen. Specifically, the one revolving around the 727 certification.
There seems to be two schools of thought to aircraft design. One is the test pilot's wet dream: simple layout, well behaved, neutral stability, or minimal bad behavior up to the corners of the flight envelope, then easily discernable, and recoverable stall behavior.
The other school is the realm of the Engineer. The Tricky Sick school if you will. Apply enough computer and piloting aid to the properly shaped brick, and it can be flown like a 737! Or Airbuses version of "let the plane fly itself, just tell it where to go."
Even as far back as the certification of the 727, test pilot's saw the shift away from the meutrally stable machine that "just flew" to an ever increasing complex mishmash of complex systems working in the background to male unstable airframes fly like naturally (neutrally) stable ones. Which is all fine and good until something goes wrong, and those systems fail, leaving a pilot in uncharted waters.
The control stick force stuff is not a distraction, just another link in the chain of normalization of deviance that resulted in a departure from "building an airworthy frame" to figuring out how to mask the "unairworthyness" of a frame sufficiently so as to get it by the regulators.
That's not to say it can't be done, but one approach is definitely inherently riskier than the other, and requires increased levels of communication among everybody involved.
Point being: this has been built up to since as far back as the 60's. See the 727 certification in above mentioned interview, the many difficulties that the MD-11 ran into with it's LSAS, and note the similar less than stellar results that emerged from trying to optimize for fuel efficiency at the cost of having to implement increasingly complex control system hacks to maintain parity with regulations/previous airframes.
Interview:
https://www.aerosociety.com/news/audio-the-d-p-davies-interv...