The 6DOF Airframe Simulink Template utilizes a multitude of constants related to the airframe and control surface aerodynamic properties. Is there documentation that exists which defines/explains the required input values?
The airframe modeled in the 6DOF template is the de Havilland Beaver. The same airframe is modeled in the Aerospace Blockset example asbdhc2. The asbdhc2 example is based on the work of Marc Rauw of Delft University of Technology - dutchroll.com (listed in the asbdhc2 model).