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

Table 3

Test results of four displacement points (unit: mm).

Load cases	Displacement measurement point (mm)
	1	2	3	4
1	5.54	5.66	4.24	4.37
2	11.68	11.56	8.76	8.76
3	11.72	11.98	8.46	8.19
4	18.98	19.24	12.83	12.69
5	26.19	25.91	16.90	17.06
6	5.64	5.78	4.35	4.11
7	11.77	11.94	8.68	8.59
8	11.80	11.65	8.39	8.51
9	18.93	18.90	12.72	12.72
10	26.20	26.02	16.81	16.74
11	5.39	5.56	4.18	4.32
12	11.82	11.84	8.73	8.99
13	11.77	11.76	8.37	8.09
14	18.99	18.74	12.76	12.78
15	26.13	25.98	16.84	16.69
16	5.51	5.35	4.28	4.24
17	17.44	17.60	12.92	12.71
18	17.66	17.44	12.55	12.37
19	28.20	28.43	18.96	18.73
20	38.69	38.58	25.33	25.39
21	62.32	62.05	42.22	42.50
22	62.45	62.67	42.26	42.05
23	62.40	62.64	42.29	42.11
24	63.41	63.23	44.02	43.94
25	63.53	63.81	44.15	44.14
26	63.20	63.12	43.93	44.02
27	-27.08	-26.68	-20.07	-20.14
28	-52.38	-51.88	-37.24	-36.89
29	-17.76	-17.84	-12.93	-12.85
30	-24.17	-23.62	-17.05	-17.42
31	-47.50	-48.35	-32.24	-31.98
32	-37.89	-38.26	-25.69	-25.33
33	-39.71	-39.53	-25.53	-25.55
34	-26.80	-26.51	-17.14	-17.24