Sets of pitch control surfaces.

Table 2: Sets of pitch control surfaces.

Figure 1	Name	Location	Area (cm²)	Area fraction to
Figure 1	Name	Location	Area (cm²)	Wing	Total Control
i = 1	Elevator	Body	27.9	0.02902	0.21816
2	Outer Elevator	Junction	17.2716	0.01797	0.13505
3	Inner flap	Inner wing	16.9428	0.001762	0.13248
4	Outer flap	Middle wing	47.4051	0.04931	0.37067
5	Aileron	Outer wing	18.36938	0.01911	0.14364
i = 0	All	Wing+body	127.889	0.13303	1.00000