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Main physical parameters of the airship have been evaluated in Table 2.
In this research, proposed branch and bound has been coded in C++ software, and its performance has been evaluated in Table 1 For each size five examples have been proposed, where all parameters have been selected randomly while creating the data set, where ( p_{j} in ;left[ {1, 10} right] ), F j ∊ [1, 10], λ j ∊ [1, 10], H ∊ [1, 10] and E ∊ [1, 10], and ( O in left[ {10,20} right] ).
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For the Fornell-Larcker Criterion, the square root of the AVE was evaluated in Table 4.
Characteristic and performance table is reported in Appendix 1, while power propulsion system is evaluated in Table 1.
For the truss studied in Example 1, accuracy of multivariate rational RS model is evaluated in Table 7.
Performance of all the methods in terms of speed is evaluated in Table 1, taken from [20].
The complexity of the precoding operation of the GFDM transceiver based on DFT algorithms are evaluated in Table 1.
For comparison purposes, its performance is evaluated in Table 3 against a known UV-NIL resist, AMO NIL MMS4.
The operational readiness of the technology, in terms of satellite data availability, robustness of methods, large-area demonstrations and country operational examples, is evaluated in Table 2.
The accuracy of these RS models is evaluated in Table 1 by means of the performance indicators described in Section 2.2. Figure 2 compares the variation of nodal displacement over the design space determined from the analytical expression (10) or by means of the three RS models.
Validation was performed using a small-scale E-MAP, and is evaluated in Table 4.
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