Application of Soft Computing Paradigm to Large Deformation Analysis of Cantilever Beam under Point Load

Table 3

Maximum and minimum absolute errors obtained in ANN-GNDO-SQP solutions for different cases of large deflection of cantilever beam.

Maximum AE	Minimum AE	Maximum AE	Minimum AE	Maximum AE	Minimum AE	Maximum AE	Minimum AE
0.0	1.07E − 08	2.16E − 10	2.54E − 08	9.14E − 11	1.28E − 07	1.30E − 10	1.24E − 07	2.18E − 09
0.1	1.03E − 08	1.67E − 10	2.18E − 08	1.36E − 10	1.06E − 07	6.97E − 10	1.46E − 07	1.48E − 09
0.2	1.02E − 08	1.82E − 10	2.46E − 08	3.53E − 11	1.27E − 07	9.89E − 12	1.41E − 07	1.72E − 09
0.3	2.23E − 10	6.59E − 12	1.20E − 09	5.38E − 12	7.64E−09	4.03E−10	2.14E − 09	8.42E − 11
0.4	4.76E − 09	7.30E − 11	8.77E − 09	5.44E − 11	4.32E−08	3.40E−10	8.23E − 08	6.09E − 10
0.5	9.86E − 09	1.73E − 10	2.25E − 08	8.30E − 11	1.20E−07	1.10E−11	1.75E−07	1.58E−09
0.6	3.79E − 09	8.09E − 11	1.11E − 08	4.73E − 11	6.36E−08	5.62E−10	7.28E−08	8.51E−10
0.7	5.26E − 10	2.83E − 12	3.14E − 10	5.72E − 13	1.06E−09	4.32E−10	8.63E − 09	1.50E − 12
0.8	1.02E − 08	1.53E − 10	2.09E − 08	1.46E − 10	1.14E−07	9.45E−11	2.06E − 07	1.08E − 09
0.9	8.53E − 09	1.56E − 10	2.22E − 08	2.44E − 10	1.28E−07	1.35E−09	1.93E − 07	1.22E − 09
1.0	1.04E − 08	1.51E − 10	2.07E − 08	2.99E − 10	1.20E−07	4.76E−10	2.30E − 07	1.24E − 09