Reconstruction of Wing Structure Deformation Based on Particle Swarm Optimization Ridge Regression

Table 1

Static load cases.

Load case	Load form	Loading point	Loading
1 ~ 15	Single point concentrated load	1 ~ 15 each load point was applied with concentrated load	10 N
16	Edge load	1, 6, 11	10 N, 10 N, 10 N
17		2, 7, 12	10 N, 10 N, 10 N
18		3, 8, 13	10 N, 10 N, 10 N
19		4, 9, 14	10 N, 10 N, 10 N
20		5, 10, 15	10 N, 10 N, 10 N
21		1, 2, 3, 4, 5	10 N, 10 N, 10 N, 10 N, 10 N
22		6, 7, 8, 9, 10	10 N, 10 N, 10 N, 10 N, 10 N
23		11, 12, 13, 14, 15	10 N, 10 N, 10 N, 10 N, 10 N
24	Gradient edge load	1, 2, 3, 4, 5	25 N, 20 N, 15 N, 10 N, 5 N
25		6,7,8,9, 10	25 N, 20 N, 15 N, 10 N, 5 N
26		11, 12, 13, 14, 15	25 N, 20 N, 15 N, 10 N, 5 N
27	Torsional load	2, 12	-50 N, 5 N
28		3, 13	-50 N, 5 N
29		3, 13	-20 N, 5 N
30		3, 13	-30 N, 10 N
31		4, 14	-30 N, 5 N
32		4, 14	-30 N, 10 N
33		5, 15	-20 N, 5 N
34		5, 15	-20 N, 10 N