Table 12 Results of the inverse scheduling method validation algorithm.

From: Inverse scheduling method for aircraft flat-tail assembly production based on improved genetic algorithm

Experimental group

Total delay time (/h)

Stability value (ES)

IS

RM

IS

RM

min

avg

min

avg

min

avg

min

avg

6X4

11

12.4

13

15.4

273

278

285

293

6X8

40

42.6

45

48.2

382

391

421

437

6X12

37

38.4

43

45.8

439

452

486

498

12X4

45

47.7

52

57.6

563

582

630

647

12X8

83

84.7

86

90.3

765

784

833

845

12X12

91

92.1

94

97.9

830

853

910

923

30X4

61

62.8

65

68.3

1086

1123

1156

1164

30X8

98

100.6

102

106.8

1235

1256

1398

1409

30X12

106

107.8

110

114.6

1387

1403

1470

1482

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