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

Table 1

The dimensions of the fence extracted from the dimensions of the wingtip vortex in millimetres.

The height of the fence (H)			The length of the fence (L)	The name of the location of the fence relative to the longitudinal axis of the UAV (distance value)
70%	50%	30%
7	5	3	49	A (158)
14	10	6	144	B (234)
22.4	16	9.6	172	C (310)