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摘要:
为进一步提高航天器等大型复杂系统的费用测算精度,将大型复杂系统看作一定参数集合的系统分布,定义待测系统与样本的Jensen-Shannon(JS)散度、灰色关联度及综合相似度,根据综合相似度计算样本权重大小,构建复杂系统费用测算的加权回归模型。当样本量较少不满足最小二乘法建模条件时,选择综合相似度最大的样本作为基准样本,构建费用的驱动效应矩阵,根据矩阵中参数与费用的JS散度大小,按序选取散度较大的参数作为测算模型的自变量。针对样本量大于和不大于参数量2种情况实例计算结果。结果表明:基于JS散度和灰色关联度融合的相似性加权回归测算模型具有较高的预测精度和稳定性。
Abstract:In order to further improve the accuracy of cost estimation for large and complex equipment, such as spacecraft and weapon systems, the large and complex equipment is regarded as a system distribution of a certain parameter set. Define the Jensen-Shannon (JS) divergence, grey correlation, and comprehensive similarity between the tested equipment and the equipment samples, and calculate the sample weight based on the similarity to construct a weighted regression model for cost estimation of complex equipment. To create the cost driving impact matrix, the sample with the highest complete similarity is chosen as the benchmark sample when the sample size does not satisfy the requirements of the least squares modeling. Based on the JS divergence between the parameters and the cost in the matrix, the parameters with larger divergence are selected as the independent variables for the prediction model. By comparing two scenarios in which the sample size is larger and smaller than the parameter size, the comparative analysis demonstrates the excellent prediction accuracy and stability of the similarity weighted regression calculation model based on the combination of JS divergence and grey correlation degree.
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Key words:
- complex equipment /
- JS divergence /
- grey correlation /
- comprehensive similarity /
- driving factor /
- accuracy /
- cost estimation
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表 1 机载电子设备费用样本
Table 1. Sample of airborne electronic equipment costs
飞机型号 首飞时间$ {x}_{1}/\text{a} $ 质量$ {x}_{2}/\text{kg} $ 体积$ {x}_{3}/{\mathrm{m}}^{3} $ 功率$ {x}_{4}/\text{kW} $ 实际平均费用
$ c $/103美元A-6E 70 624.25 0.5691 6.4 1069 A-7D 68 508.25 0.7101 10.5 669 F-4D 65 790.41 0.8430 8.2 582 A-10A 72 265.14 0.2394 3.1 315 E-4E 67 566.14 0.6773 5.3 662 F-4J 66 1021.05 0.9824 19.4 1329 F-15A 72 717.32 0.8331 22.5 2488 F-111A 64 805.40 0.8774 5.6 1267 F-111D 68 1068.72 0.9102 12.5 2392 F-111F 71 933.88 1.0611 8.9 1577 FB-111A 70 1136.36 1.3432 7.9 1965 F-14A 70 998.35 1.0628 29.4 2383 A-7E 68 653.76 0.8413 8.3 828 F-111E 69 987.00 1.1054 8.9 1564 表 2 3个待预测机载电子设备综合相似度和权重
Table 2. Comprehensive similarity and weight of three predicted airborne electronic devices
飞机型号 相似度 权重 与F-14A对比 与A-7E对比 与F-111E对比 与F-14A对比 与A-7E对比 与F-111E对比 A-6E 0.77 0.85 0.80 0.09 0.10 0.09 A-7D 0.76 0.90 0.81 0.09 0.10 0.09 F-4D 0.75 0.88 0.82 0.09 0.10 0.09 A-10A 0.52 0.55 0.53 0.06 0.06 0.06 E-4E 0.73 0.87 0.78 0.09 0.10 0.09 F-4J 0.85 0.75 0.81 0.10 0.08 0.09 F-15A 0.82 0.81 0.74 0.10 0.09 0.08 F-111A 0.70 0.78 0.76 0.08 0.09 0.09 F-111D 0.83 0.86 0.87 0.10 0.10 0.10 F-111F 0.86 0.82 0.92 0.10 0.09 0.11 FB-111A 0.82 0.79 0.88 0.10 0.09 0.10 表 3 4种预测方法的结果比较
Table 3. Result comparison of four prediction methods
万元 表 4 4种预测方法的预测误差比较
Table 4. Comparison of prediction errors among four prediction methods
表 5 运输机性能数据与费用
Table 5. Performance data and cost of transport aircraft
飞机型号 最大起飞质量
$ {x}_{1}/\text{kg} $机身长
$ {x}_{2}/\text{m} $机高
$ {x}_{3}/\text{m} $起飞距离
$ {x}_{4}/\text{m} $满油航程
$ {x}_{5}/\text{km} $最大平飞速度
$ {x}_{6}/(\text{m}\cdot {\text{s}}^{{-1}}) $空重
$ {x}_{7}/\text{kg} $载油量
$ {x}_{8}/\text{kg} $费用
$ c $/万元A 13494 23.500 8.43 867 4262 425.0 6597 5683 6666.70 B 6849 14.390 4.57 987 3701 746.0 3655 2640 3524.30 C 9979 16.900 5.12 1581 4679 874.0 5357 3350 6569.90 D 5670 13.340 4.57 536 3641 536.0 3656 1653 5586.23 E 63503 39.750 9.30 1859 6764 925.0 33183 21273 27768.80 F 22000 29.870 6.75 1200 2870 907.0 34360 5500 17575.20 G 21500 27.170 7.65 1050 2000 580.0 12200 5000 18137.60 H 70310 29.790 11.66 1091 7876 602.0 36300 36300 50476.00 I 21000 24.615 7.30 1300 3100 819.2 11700 6000 14250.00 -
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