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aerodynamic state space model

aerodynamic state space model

(OP)
Hello
I'm studying the stability of a particular aircraft and need the coefficients/values (not the aerodynamic derivatives) of the state-space matrix (system matrix in particular) for a cessna 172, altitude around 5000 ft and speed around 220 fps to validate my aircraft model on matlab.
Do you know how I can get that?
I'm also interested in other state space model data for other airplanes.
Thanks for your tipps
Hugues

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