A Unified Approach to Nonlinear Dynamic Inversion Control with Parameter Determination by Eigenvalue Assignment

Table 1

The geometric data, weight, and moment of inertia of the UAV.

	Parameter	Value	Units
Reference wing area			ft^2
Wing span			ft
Mean aerodynamic chord			ft
Weight			lb
-axis inertia			slug/ft^2
-axis inertia			slug/ft^2
-axis inertia			slug/ft^2
- product of inertia			slug/ft^2