DC8:

Path: AC/Aircraft

% DC 8 stability derivatives model.
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   Form:
   x = DC8( q, n )
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   ------
   Inputs
   ------
   q                      String describing the type of data
   n                      Set

   -------
   Outputs
   -------
   x                      The properties

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   Reference: McRuer, D., Ashenas, I., and D. Graham, Aircraft Dynamics 
              and Automatic Control, Princeton, 1973, pp. 711-714
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