Kriging and Radial Basis Function Models for Optimized Design of UAV Wing Fences to Reduce Rolling Moment

Table 2

The exact dimensions of the fences created on the UAV wing at three different heights and the optimized point (O) in millimetres.

Fence height (H)			The distance between the fence and the nose of the UAV (D)	The length of the fence (L)	The name of the fence (distance from the longitudinal axis)
70% P	50% P	30% P
7	5	3	280	49	(158)-A
14	10	6	447	144	(234)-B
22.4	16	9.6	581	172	(310)-C
		7.5	435	121	(236)-O
	13		460	149	(240)-O
18.2			543	163	(290)-O