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What's the relation between limit of deflection for aerodynamic control surfaces (tail control) and altitude for surface to air missiles?

Also how can the fin deflection range (Max/Min) be determined for any altitude?

Please mention any reference text related to the subject.

DeltaLima
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Madox
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    From Missile Guidance and Control Systems by George M. Siouris, I know that Maximum fin deflection is limited by the missile velocity and the altitude band in which the missile is flying but i cant find any procedure to determine this upper limit. – Madox Dec 25 '17 at 21:52

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