International Journal of Fuzzy Logic and Intelligent Systems 2018; 18(4): 237-244
Published online December 31, 2018
https://doi.org/10.5391/IJFIS.2018.18.4.237
© The Korean Institute of Intelligent Systems
Zong Woo Geem, and Jin-Hong Kim
1Department of Energy IT, Gachon University, Seongnam, Korea, 2Department of Civil & Environmental Engineering, Chung-Ang University, Seoul, Korea
Correspondence to :
Jin-Hong Kim, (jinhong.kim.cau@gmail.com)
This is an Open Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/3.0/) which permits unrestricted noncommercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
Manning formula is one of the most famous functions used in hydraulics and hydrology, which calculates the average flow velocity based on roughness coefficient, hydraulic radius, and slope. This study intends to improve the original formula by minimizing the deviation error between calculated flow velocity and observed one. The first improvement approach was to estimate the exponent values of hydraulic radius and slope, instead of using current 2/3 and 1/2, while fixing the roughness value. When logarithm-converted multiple linear regression, calculus-based BFGS technique, and meta-heuristic genetic algorithm were applied to the problem, genetic algorithm found the best exponent values in terms of sum of squares error and coefficient of determination. The second approach was to estimate the individual roughness value, instead of a constant one, which is the function of hydraulic radius and slope. When multiple linear regression, artificial neural network with BFGS, and artificial neural network with genetic algorithm tackled the problem, the latter found the best solution. We hope these approaches will be utilized more practically in the future.
Keywords: Computational intelligence, Manning equation, Hydraulics, Curve fitting, Genetic algorithm, Artificial neural network
The Manning formula, also referred to as Gauckler-Manning formula (or Gauckler-Manning-Strickler formula) in Europe [1] or Manning’s equation in the United States [2] and English-speaking countries [3], is a simple-structured empirical formula which calculates the average velocity of uniform or gradually varied flow [2] in an open channel. The common form of the formula is
where
The Manning formula is utilized for fully rough turbulent flows [1] and is usually applied to free surface profile calculation in an open channel or circular-piped sewer design [2].
This empirical formula sometimes does not work very well because it is sensitive to roughness value
If the Manning’s roughness coefficient
Also,
In order to find fixed
In this situation, is there any way to further improve the Manning formula with fixed roughness coefficient? For this “empirical” formula, the exponent values, such as 2/3 of hydraulic radius and 1/2 of slope, appear somewhat arbitrary and those values can be optimized using several techniques [10] such as multiple linear regression (MLR), calculus-based optimization, and meta-heuristic optimization.
For an optimal exponent estimation using MLR, we can first apply a logarithm to both sides of
And, the common form of MLR is
Since we already have the dataset of
The regression result shows that
Instead of using the above logarithm-converted multiple linear regression (Ln-MLR), we can adopt optimization techniques for estimating the roughness coefficient and two exponent values. In this optimization process, we have to minimize the sum of squares error (SSE) as follows:
where
When a calculus-based optimization technique, named BFGS [11], was applied to the identical dataset, we could obtain
When a popular meta-heuristic algorithm, named genetic algorithm (GA) [12], was also applied to the identical dataset, we could obtain
Roughness value
If the Manning’s roughness coefficient
The individual roughness value is shown in the third column of Table 3. When a graph of
Furthermore, when a graph of
With the above relationships among hydraulic radius, slope and roughness, we can derive a two-independent-variable function using MLR as follows:
MLR could obtain
In the varied roughness approach by MLR, the roughness
This study introduces an artificial neural network (ANN) approach with optimization technique, which can consider non-linearity among variables. Actually ANN approaches have been applied to various prediction problems such as energy demand [17] or water pipe deterioration [18]. While those approaches used error-back-propagation technique to adjust the weight values among layers, a recent ANN approach hybridized ANN with an optimization algorithm to search the solution space of an ocean engineering problem more efficiently [19]. The basic ANN model, named feed-forward multilayer perceptron, can be structured as shown in Figure 6. As shown in the figure, there are three layers (input layer in left column, hidden layer in middle column, and output layer in right column). If we put certain values for hydraulic radius
When the ANN was hybridized with BFGS (ANN+BFGS), this model slightly enhanced the solution quality when compared with MLR, obtaining
When the ANN was hybridized with GA (ANN+GA), this model even enhanced the solution quality when compared with ANN+BFGS, obtaining
The amount of data (26 points) introduced in Table 1 does not appear very large. Nonetheless, this is not small for our regression-type neural-network calculation. In fact, a much larger dataset is required for unstructured data (pixel-type photos or sound wave files). However, because our hydraulic data is very structured (number-type), 26 points might be enough for devising the better formula, which could be verified with statistical indexes (
Actually, Manning formula can be derived from Chézy formula [13] as follows:
where
Since the basic structure of the Chézy formula relies on a physical relationship between the average velocity and the square root of the bed shear stress (
Manning formula is usually used by engineers, who barely have much knowledge of cutting-edge computational intelligence techniques, such as artificial neural network and genetic algorithm. The ANN model in this study can be simply an improved model which considers higher nonlinearity between independent variables and a dependent one, than existing MLR model. And, the GA technique can be utilized for globally finding optimal weighting values of the ANN model. However, a calculus-based BFGS model, which finds optimal weighting values locally, could perform as well as GA in this study. In order for engineers to easily use these techniques, application software can be coded in the form of spreadsheet macros.
This study proposed various techniques to improve the original Manning formula. The approach was divided into two parts. The first approach was to estimate the exponents of hydraulic radius and slope while fixing the roughness value. When three different techniques, such as logarithm-converted MLR, gradient-based BFGS, and meta-heuristic GA as well as zero-intercept LR, tackled the problem, the GA technique found the best solutions with respect to determination coefficient and SSE.
The second approach was to estimate the individual roughness value while fixing the exponent values of hydraulic radius and slope. When three different techniques, such as MLR, ANN+BFGS, and ANN+GA, tackled the problem, ANN+GA found the best solutions with respect to determination coefficient and SSE.
Nonetheless, we have to admit that this study has a limitation when determining the Manning’s roughness
The authors declare no conflict of interest.
Table 1. Experimental dataset and calculated velocities with fixed
Run No. | |||||||
---|---|---|---|---|---|---|---|
0I-LR | Ln-MLR | BFGS | GA | ||||
1 | 0.400945 | 0.060583 | 0.00113 | 0.384760 | 0.421653 | 0.427683 | 0.424328 |
2 | 0.440086 | 0.070916 | 0.00112 | 0.425455 | 0.475809 | 0.481878 | 0.480858 |
3 | 0.493025 | 0.073364 | 0.00113 | 0.437130 | 0.490042 | 0.495939 | 0.495704 |
4 | 0.557127 | 0.078054 | 0.00112 | 0.453548 | 0.513028 | 0.518989 | 0.519815 |
5 | 0.340164 | 0.044717 | 0.00167 | 0.382025 | 0.376098 | 0.377570 | 0.375687 |
6 | 0.421810 | 0.056999 | 0.00167 | 0.449112 | 0.455053 | 0.455539 | 0.457541 |
7 | 0.443044 | 0.066841 | 0.00165 | 0.496423 | 0.513707 | 0.513518 | 0.518728 |
8 | 0.540074 | 0.074797 | 0.00165 | 0.535074 | 0.561139 | 0.560194 | 0.568344 |
9 | 0.263983 | 0.019121 | 0.00332 | 0.305722 | 0.240101 | 0.237589 | 0.234723 |
10 | 0.304127 | 0.026482 | 0.00331 | 0.379283 | 0.309773 | 0.305399 | 0.305505 |
11 | 0.379098 | 0.032199 | 0.00333 | 0.433381 | 0.361859 | 0.355859 | 0.358765 |
12 | 0.454098 | 0.039972 | 0.00333 | 0.500578 | 0.428822 | 0.420646 | 0.427642 |
13 | 0.369026 | 0.060583 | 0.00111 | 0.381340 | 0.419267 | 0.425533 | 0.421913 |
14 | 0.401014 | 0.062495 | 0.00112 | 0.391069 | 0.430846 | 0.436987 | 0.433936 |
15 | 0.438431 | 0.065183 | 0.00113 | 0.403997 | 0.446593 | 0.452592 | 0.450315 |
16 | 0.561799 | 0.073882 | 0.00112 | 0.437237 | 0.491367 | 0.497396 | 0.497130 |
17 | 0.565847 | 0.074797 | 0.00112 | 0.440840 | 0.496139 | 0.502155 | 0.502126 |
18 | 0.363013 | 0.038834 | 0.00168 | 0.348775 | 0.337300 | 0.339108 | 0.335656 |
19 | 0.430440 | 0.051457 | 0.00165 | 0.416984 | 0.418323 | 0.419451 | 0.419442 |
20 | 0.477283 | 0.055201 | 0.00167 | 0.439616 | 0.443742 | 0.444382 | 0.445783 |
21 | 0.500336 | 0.059032 | 0.00166 | 0.458349 | 0.466857 | 0.467263 | 0.469848 |
22 | 0.556912 | 0.064065 | 0.00167 | 0.485498 | 0.498785 | 0.498636 | 0.503096 |
23 | 0.282029 | 0.024382 | 0.00333 | 0.360036 | 0.290865 | 0.286975 | 0.286223 |
24 | 0.283186 | 0.025394 | 0.00332 | 0.369376 | 0.300019 | 0.295897 | 0.295552 |
25 | 0.383270 | 0.034578 | 0.00331 | 0.453106 | 0.381960 | 0.375394 | 0.379418 |
26 | 0.394911 | 0.040649 | 0.00332 | 0.505460 | 0.434107 | 0.425792 | 0.433106 |
Table 2. Optimal parameter values from various techniques.
Method | SSE | ||||
---|---|---|---|---|---|
0I-LR | 0.6667 | 0.5000 | 0.0135 | 0.4861 | 0.1041 |
Ln-MLR | 0.7853 | 0.3178 | 0.0304 | 0.8294 | 0.0347 |
BFGS | 0.7736 | 0.2823 | 0.0394 | 0.8295 | 0.0345 |
GA | 0.8122 | 0.3197 | 0.0276 | 0.8309 | 0.0342 |
Table 3. Experimental dataset and calculated velocities with varied
Run No. | ||||||||
---|---|---|---|---|---|---|---|---|
MLR | ANN+BFGS | ANN+GA | MLR | ANN+BFGS | ANN+GA | |||
1 | 0.400945 | 0.012933 | 0.412319 | 0.418819 | 0.410950 | 0.012576 | 0.012381 | 0.012618 |
2 | 0.440086 | 0.013029 | 0.473793 | 0.487133 | 0.471736 | 0.012102 | 0.011770 | 0.012155 |
3 | 0.493025 | 0.011949 | 0.490799 | 0.505732 | 0.496809 | 0.012003 | 0.011649 | 0.011858 |
4 | 0.557127 | 0.010971 | 0.518795 | 0.538541 | 0.585896 | 0.011782 | 0.011350 | 0.010432 |
5 | 0.340164 | 0.015135 | 0.370899 | 0.364315 | 0.379831 | 0.013881 | 0.014132 | 0.013555 |
6 | 0.421810 | 0.014349 | 0.454040 | 0.445487 | 0.453332 | 0.013330 | 0.013586 | 0.013351 |
7 | 0.443044 | 0.015100 | 0.519934 | 0.512035 | 0.509077 | 0.012867 | 0.013066 | 0.013142 |
8 | 0.540074 | 0.013352 | 0.576392 | 0.570223 | 0.560367 | 0.012511 | 0.012646 | 0.012868 |
9 | 0.263983 | 0.015608 | 0.244620 | 0.252857 | 0.254519 | 0.016843 | 0.016294 | 0.016188 |
10 | 0.304127 | 0.016807 | 0.309751 | 0.315694 | 0.316054 | 0.016502 | 0.016191 | 0.016173 |
11 | 0.379098 | 0.015406 | 0.359028 | 0.362360 | 0.361278 | 0.016268 | 0.016118 | 0.016166 |
12 | 0.454098 | 0.014856 | 0.423771 | 0.421844 | 0.417734 | 0.015919 | 0.015992 | 0.016149 |
13 | 0.369026 | 0.013926 | 0.409370 | 0.416470 | 0.407822 | 0.012554 | 0.012340 | 0.012602 |
14 | 0.401014 | 0.013143 | 0.422327 | 0.430116 | 0.419148 | 0.012479 | 0.012253 | 0.012574 |
15 | 0.438431 | 0.012418 | 0.440150 | 0.449151 | 0.435160 | 0.012370 | 0.012122 | 0.012512 |
16 | 0.561799 | 0.010489 | 0.492323 | 0.508122 | 0.502058 | 0.011969 | 0.011597 | 0.011737 |
17 | 0.565847 | 0.010499 | 0.498087 | 0.514702 | 0.514645 | 0.011928 | 0.011543 | 0.011544 |
18 | 0.363013 | 0.012948 | 0.332046 | 0.326778 | 0.343594 | 0.014156 | 0.014384 | 0.013680 |
19 | 0.430440 | 0.013055 | 0.414518 | 0.406985 | 0.419285 | 0.013557 | 0.013808 | 0.013403 |
20 | 0.477283 | 0.012413 | 0.441769 | 0.433391 | 0.442782 | 0.013411 | 0.013670 | 0.013380 |
21 | 0.500336 | 0.012346 | 0.466955 | 0.458501 | 0.464440 | 0.013228 | 0.013472 | 0.013300 |
22 | 0.556912 | 0.011749 | 0.502771 | 0.494049 | 0.494495 | 0.013014 | 0.013243 | 0.013232 |
23 | 0.282029 | 0.017204 | 0.291977 | 0.298950 | 0.299863 | 0.016618 | 0.016231 | 0.016181 |
24 | 0.283186 | 0.017578 | 0.300571 | 0.307062 | 0.307717 | 0.016562 | 0.016212 | 0.016177 |
25 | 0.383270 | 0.015932 | 0.378361 | 0.380001 | 0.377960 | 0.016139 | 0.016069 | 0.016156 |
26 | 0.394911 | 0.017249 | 0.429020 | 0.426441 | 0.421927 | 0.015878 | 0.015974 | 0.016145 |
E-mail: zwgeem@gmail.com
E-mail: jinhong.kim.cau@gmail.com
International Journal of Fuzzy Logic and Intelligent Systems 2018; 18(4): 237-244
Published online December 31, 2018 https://doi.org/10.5391/IJFIS.2018.18.4.237
Copyright © The Korean Institute of Intelligent Systems.
Zong Woo Geem, and Jin-Hong Kim
1Department of Energy IT, Gachon University, Seongnam, Korea, 2Department of Civil & Environmental Engineering, Chung-Ang University, Seoul, Korea
Correspondence to: Jin-Hong Kim, (jinhong.kim.cau@gmail.com)
This is an Open Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/3.0/) which permits unrestricted noncommercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
Manning formula is one of the most famous functions used in hydraulics and hydrology, which calculates the average flow velocity based on roughness coefficient, hydraulic radius, and slope. This study intends to improve the original formula by minimizing the deviation error between calculated flow velocity and observed one. The first improvement approach was to estimate the exponent values of hydraulic radius and slope, instead of using current 2/3 and 1/2, while fixing the roughness value. When logarithm-converted multiple linear regression, calculus-based BFGS technique, and meta-heuristic genetic algorithm were applied to the problem, genetic algorithm found the best exponent values in terms of sum of squares error and coefficient of determination. The second approach was to estimate the individual roughness value, instead of a constant one, which is the function of hydraulic radius and slope. When multiple linear regression, artificial neural network with BFGS, and artificial neural network with genetic algorithm tackled the problem, the latter found the best solution. We hope these approaches will be utilized more practically in the future.
Keywords: Computational intelligence, Manning equation, Hydraulics, Curve fitting, Genetic algorithm, Artificial neural network
The Manning formula, also referred to as Gauckler-Manning formula (or Gauckler-Manning-Strickler formula) in Europe [1] or Manning’s equation in the United States [2] and English-speaking countries [3], is a simple-structured empirical formula which calculates the average velocity of uniform or gradually varied flow [2] in an open channel. The common form of the formula is
where
The Manning formula is utilized for fully rough turbulent flows [1] and is usually applied to free surface profile calculation in an open channel or circular-piped sewer design [2].
This empirical formula sometimes does not work very well because it is sensitive to roughness value
If the Manning’s roughness coefficient
Also,
In order to find fixed
In this situation, is there any way to further improve the Manning formula with fixed roughness coefficient? For this “empirical” formula, the exponent values, such as 2/3 of hydraulic radius and 1/2 of slope, appear somewhat arbitrary and those values can be optimized using several techniques [10] such as multiple linear regression (MLR), calculus-based optimization, and meta-heuristic optimization.
For an optimal exponent estimation using MLR, we can first apply a logarithm to both sides of
And, the common form of MLR is
Since we already have the dataset of
The regression result shows that
Instead of using the above logarithm-converted multiple linear regression (Ln-MLR), we can adopt optimization techniques for estimating the roughness coefficient and two exponent values. In this optimization process, we have to minimize the sum of squares error (SSE) as follows:
where
When a calculus-based optimization technique, named BFGS [11], was applied to the identical dataset, we could obtain
When a popular meta-heuristic algorithm, named genetic algorithm (GA) [12], was also applied to the identical dataset, we could obtain
Roughness value
If the Manning’s roughness coefficient
The individual roughness value is shown in the third column of Table 3. When a graph of
Furthermore, when a graph of
With the above relationships among hydraulic radius, slope and roughness, we can derive a two-independent-variable function using MLR as follows:
MLR could obtain
In the varied roughness approach by MLR, the roughness
This study introduces an artificial neural network (ANN) approach with optimization technique, which can consider non-linearity among variables. Actually ANN approaches have been applied to various prediction problems such as energy demand [17] or water pipe deterioration [18]. While those approaches used error-back-propagation technique to adjust the weight values among layers, a recent ANN approach hybridized ANN with an optimization algorithm to search the solution space of an ocean engineering problem more efficiently [19]. The basic ANN model, named feed-forward multilayer perceptron, can be structured as shown in Figure 6. As shown in the figure, there are three layers (input layer in left column, hidden layer in middle column, and output layer in right column). If we put certain values for hydraulic radius
When the ANN was hybridized with BFGS (ANN+BFGS), this model slightly enhanced the solution quality when compared with MLR, obtaining
When the ANN was hybridized with GA (ANN+GA), this model even enhanced the solution quality when compared with ANN+BFGS, obtaining
The amount of data (26 points) introduced in Table 1 does not appear very large. Nonetheless, this is not small for our regression-type neural-network calculation. In fact, a much larger dataset is required for unstructured data (pixel-type photos or sound wave files). However, because our hydraulic data is very structured (number-type), 26 points might be enough for devising the better formula, which could be verified with statistical indexes (
Actually, Manning formula can be derived from Chézy formula [13] as follows:
where
Since the basic structure of the Chézy formula relies on a physical relationship between the average velocity and the square root of the bed shear stress (
Manning formula is usually used by engineers, who barely have much knowledge of cutting-edge computational intelligence techniques, such as artificial neural network and genetic algorithm. The ANN model in this study can be simply an improved model which considers higher nonlinearity between independent variables and a dependent one, than existing MLR model. And, the GA technique can be utilized for globally finding optimal weighting values of the ANN model. However, a calculus-based BFGS model, which finds optimal weighting values locally, could perform as well as GA in this study. In order for engineers to easily use these techniques, application software can be coded in the form of spreadsheet macros.
This study proposed various techniques to improve the original Manning formula. The approach was divided into two parts. The first approach was to estimate the exponents of hydraulic radius and slope while fixing the roughness value. When three different techniques, such as logarithm-converted MLR, gradient-based BFGS, and meta-heuristic GA as well as zero-intercept LR, tackled the problem, the GA technique found the best solutions with respect to determination coefficient and SSE.
The second approach was to estimate the individual roughness value while fixing the exponent values of hydraulic radius and slope. When three different techniques, such as MLR, ANN+BFGS, and ANN+GA, tackled the problem, ANN+GA found the best solutions with respect to determination coefficient and SSE.
Nonetheless, we have to admit that this study has a limitation when determining the Manning’s roughness
Relationship plot of fixed roughness coefficient.
Relationship plot using multiple linear regression.
Relationship plot between hydraulic radius and roughness.
Relationship plot between slope and roughness.
Observed and calculated velocities from MLR.
Structure of feed-forward multilayer perceptron model.
Table 1 . Experimental dataset and calculated velocities with fixed
Run No. | |||||||
---|---|---|---|---|---|---|---|
0I-LR | Ln-MLR | BFGS | GA | ||||
1 | 0.400945 | 0.060583 | 0.00113 | 0.384760 | 0.421653 | 0.427683 | 0.424328 |
2 | 0.440086 | 0.070916 | 0.00112 | 0.425455 | 0.475809 | 0.481878 | 0.480858 |
3 | 0.493025 | 0.073364 | 0.00113 | 0.437130 | 0.490042 | 0.495939 | 0.495704 |
4 | 0.557127 | 0.078054 | 0.00112 | 0.453548 | 0.513028 | 0.518989 | 0.519815 |
5 | 0.340164 | 0.044717 | 0.00167 | 0.382025 | 0.376098 | 0.377570 | 0.375687 |
6 | 0.421810 | 0.056999 | 0.00167 | 0.449112 | 0.455053 | 0.455539 | 0.457541 |
7 | 0.443044 | 0.066841 | 0.00165 | 0.496423 | 0.513707 | 0.513518 | 0.518728 |
8 | 0.540074 | 0.074797 | 0.00165 | 0.535074 | 0.561139 | 0.560194 | 0.568344 |
9 | 0.263983 | 0.019121 | 0.00332 | 0.305722 | 0.240101 | 0.237589 | 0.234723 |
10 | 0.304127 | 0.026482 | 0.00331 | 0.379283 | 0.309773 | 0.305399 | 0.305505 |
11 | 0.379098 | 0.032199 | 0.00333 | 0.433381 | 0.361859 | 0.355859 | 0.358765 |
12 | 0.454098 | 0.039972 | 0.00333 | 0.500578 | 0.428822 | 0.420646 | 0.427642 |
13 | 0.369026 | 0.060583 | 0.00111 | 0.381340 | 0.419267 | 0.425533 | 0.421913 |
14 | 0.401014 | 0.062495 | 0.00112 | 0.391069 | 0.430846 | 0.436987 | 0.433936 |
15 | 0.438431 | 0.065183 | 0.00113 | 0.403997 | 0.446593 | 0.452592 | 0.450315 |
16 | 0.561799 | 0.073882 | 0.00112 | 0.437237 | 0.491367 | 0.497396 | 0.497130 |
17 | 0.565847 | 0.074797 | 0.00112 | 0.440840 | 0.496139 | 0.502155 | 0.502126 |
18 | 0.363013 | 0.038834 | 0.00168 | 0.348775 | 0.337300 | 0.339108 | 0.335656 |
19 | 0.430440 | 0.051457 | 0.00165 | 0.416984 | 0.418323 | 0.419451 | 0.419442 |
20 | 0.477283 | 0.055201 | 0.00167 | 0.439616 | 0.443742 | 0.444382 | 0.445783 |
21 | 0.500336 | 0.059032 | 0.00166 | 0.458349 | 0.466857 | 0.467263 | 0.469848 |
22 | 0.556912 | 0.064065 | 0.00167 | 0.485498 | 0.498785 | 0.498636 | 0.503096 |
23 | 0.282029 | 0.024382 | 0.00333 | 0.360036 | 0.290865 | 0.286975 | 0.286223 |
24 | 0.283186 | 0.025394 | 0.00332 | 0.369376 | 0.300019 | 0.295897 | 0.295552 |
25 | 0.383270 | 0.034578 | 0.00331 | 0.453106 | 0.381960 | 0.375394 | 0.379418 |
26 | 0.394911 | 0.040649 | 0.00332 | 0.505460 | 0.434107 | 0.425792 | 0.433106 |
Table 2 . Optimal parameter values from various techniques.
Method | SSE | ||||
---|---|---|---|---|---|
0I-LR | 0.6667 | 0.5000 | 0.0135 | 0.4861 | 0.1041 |
Ln-MLR | 0.7853 | 0.3178 | 0.0304 | 0.8294 | 0.0347 |
BFGS | 0.7736 | 0.2823 | 0.0394 | 0.8295 | 0.0345 |
GA | 0.8122 | 0.3197 | 0.0276 | 0.8309 | 0.0342 |
Table 3 . Experimental dataset and calculated velocities with varied
Run No. | ||||||||
---|---|---|---|---|---|---|---|---|
MLR | ANN+BFGS | ANN+GA | MLR | ANN+BFGS | ANN+GA | |||
1 | 0.400945 | 0.012933 | 0.412319 | 0.418819 | 0.410950 | 0.012576 | 0.012381 | 0.012618 |
2 | 0.440086 | 0.013029 | 0.473793 | 0.487133 | 0.471736 | 0.012102 | 0.011770 | 0.012155 |
3 | 0.493025 | 0.011949 | 0.490799 | 0.505732 | 0.496809 | 0.012003 | 0.011649 | 0.011858 |
4 | 0.557127 | 0.010971 | 0.518795 | 0.538541 | 0.585896 | 0.011782 | 0.011350 | 0.010432 |
5 | 0.340164 | 0.015135 | 0.370899 | 0.364315 | 0.379831 | 0.013881 | 0.014132 | 0.013555 |
6 | 0.421810 | 0.014349 | 0.454040 | 0.445487 | 0.453332 | 0.013330 | 0.013586 | 0.013351 |
7 | 0.443044 | 0.015100 | 0.519934 | 0.512035 | 0.509077 | 0.012867 | 0.013066 | 0.013142 |
8 | 0.540074 | 0.013352 | 0.576392 | 0.570223 | 0.560367 | 0.012511 | 0.012646 | 0.012868 |
9 | 0.263983 | 0.015608 | 0.244620 | 0.252857 | 0.254519 | 0.016843 | 0.016294 | 0.016188 |
10 | 0.304127 | 0.016807 | 0.309751 | 0.315694 | 0.316054 | 0.016502 | 0.016191 | 0.016173 |
11 | 0.379098 | 0.015406 | 0.359028 | 0.362360 | 0.361278 | 0.016268 | 0.016118 | 0.016166 |
12 | 0.454098 | 0.014856 | 0.423771 | 0.421844 | 0.417734 | 0.015919 | 0.015992 | 0.016149 |
13 | 0.369026 | 0.013926 | 0.409370 | 0.416470 | 0.407822 | 0.012554 | 0.012340 | 0.012602 |
14 | 0.401014 | 0.013143 | 0.422327 | 0.430116 | 0.419148 | 0.012479 | 0.012253 | 0.012574 |
15 | 0.438431 | 0.012418 | 0.440150 | 0.449151 | 0.435160 | 0.012370 | 0.012122 | 0.012512 |
16 | 0.561799 | 0.010489 | 0.492323 | 0.508122 | 0.502058 | 0.011969 | 0.011597 | 0.011737 |
17 | 0.565847 | 0.010499 | 0.498087 | 0.514702 | 0.514645 | 0.011928 | 0.011543 | 0.011544 |
18 | 0.363013 | 0.012948 | 0.332046 | 0.326778 | 0.343594 | 0.014156 | 0.014384 | 0.013680 |
19 | 0.430440 | 0.013055 | 0.414518 | 0.406985 | 0.419285 | 0.013557 | 0.013808 | 0.013403 |
20 | 0.477283 | 0.012413 | 0.441769 | 0.433391 | 0.442782 | 0.013411 | 0.013670 | 0.013380 |
21 | 0.500336 | 0.012346 | 0.466955 | 0.458501 | 0.464440 | 0.013228 | 0.013472 | 0.013300 |
22 | 0.556912 | 0.011749 | 0.502771 | 0.494049 | 0.494495 | 0.013014 | 0.013243 | 0.013232 |
23 | 0.282029 | 0.017204 | 0.291977 | 0.298950 | 0.299863 | 0.016618 | 0.016231 | 0.016181 |
24 | 0.283186 | 0.017578 | 0.300571 | 0.307062 | 0.307717 | 0.016562 | 0.016212 | 0.016177 |
25 | 0.383270 | 0.015932 | 0.378361 | 0.380001 | 0.377960 | 0.016139 | 0.016069 | 0.016156 |
26 | 0.394911 | 0.017249 | 0.429020 | 0.426441 | 0.421927 | 0.015878 | 0.015974 | 0.016145 |
Tien Anh Tran
International Journal of Fuzzy Logic and Intelligent Systems 2024; 24(3): 306-316 https://doi.org/10.5391/IJFIS.2024.24.3.306Jeong-Hun Kang, Seong-Jin Park, Ye-Won Kim, and Bo-Yeong Kang
International Journal of Fuzzy Logic and Intelligent Systems 2024; 24(3): 242-257 https://doi.org/10.5391/IJFIS.2024.24.3.242Amirthalakshmi Thirumalai Maadapoosi, Velan Balamurugan, V. Vedanarayanan, Sahaya Anselin Nisha, and R. Narmadha
International Journal of Fuzzy Logic and Intelligent Systems 2024; 24(3): 231-241 https://doi.org/10.5391/IJFIS.2024.24.3.231Relationship plot of fixed roughness coefficient.
|@|~(^,^)~|@|Relationship plot using multiple linear regression.
|@|~(^,^)~|@|Relationship plot between hydraulic radius and roughness.
|@|~(^,^)~|@|Relationship plot between slope and roughness.
|@|~(^,^)~|@|Observed and calculated velocities from MLR.
|@|~(^,^)~|@|Structure of feed-forward multilayer perceptron model.