I understand the definition of aircraft 'Stability-Axis', but I am unsure as to the circumstances in which forces or moments would be expressed in this axis system. Is there a convention?
What I do know:
- It is useful for wind tunnel analysis, where forces and moments are often calculated from a force balance fixed to the aircraft that is invariant with model Alpha and Yaws with the aircraft for variations in Beta. (Obviously depending on windtunnel/model set-up).
- It can be used as an approximation for Wind-Axis is Alpha is known and Beta is assumed to be small.
What I don't know:
- Many things
- Why Stability-Axis is used instead of Body-Axis or Wind-Axis?
