Anti-sophist
Graduate Poster
- Joined
- Sep 15, 2006
- Messages
- 1,542
Even with large changes in pitch an accelerometer essentially measures the acceleration perpendicular to the earth. This is most important in maneuvering as this is the most significant stress on an aircraft. The most significant longitudinal stress would be from engine power and even in an F-15 or F-22 in full afterburner this would not produce anything even close to excessive stress.
For the record, the aircraft has a 3-axes accelerometer and measures all three: longitudinal, lateral, and vertical. All three measurements are present in the FDR data.
Regarding accelerations - what would vertical acceleration show if the plane was flying upside down?
I like this question. I'm fairly certain that the answer should be -1 G. In order to remain in level flight, upside down, the plane (and the people inside) must exert their own weight worth of force in the opposite direction "as usual".
In this case, "positive" G is defined as directly up relative to the plane of the aircraft. In normal level flight, you exert your own weight upward, relative to the aircraft. In upside down flight, you'd exert that force downward, relative to the aircraft.
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