Nothing Special   »   [go: up one dir, main page]

You seem to have javascript disabled. Please note that many of the page functionalities won't work as expected without javascript enabled.
 
 
Sign in to use this feature.

Years

Between: -

Subjects

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Journals

Article Types

Countries / Regions

remove_circle_outline
remove_circle_outline
remove_circle_outline

Search Results (233)

Search Parameters:
Keywords = Newton–Raphson method

Order results
Result details
Results per page
Select all
Export citation of selected articles as:
17 pages, 1355 KiB  
Article
Lubrication Analysis of a Mechanical Seal Considering the Mixed Lubricant State of Gas and Liquid During External Power Shutdown of a Reactor Cooling Pump
by Youngjun Park, Gwanghee Hong, Sanghyun Jun, Jeongmook Choi, Taegyu Kim, Minsoo Kang and Gunhee Jang
Lubricants 2024, 12(12), 406; https://doi.org/10.3390/lubricants12120406 - 21 Nov 2024
Abstract
We proposed a method to calculate the pressure, opening force, and leakage rate in a mechanical seal under the mixed lubricant state of a gas and liquid for the mechanical seal in a reactor cooling pump (RCP) during external power loss. We calculated [...] Read more.
We proposed a method to calculate the pressure, opening force, and leakage rate in a mechanical seal under the mixed lubricant state of a gas and liquid for the mechanical seal in a reactor cooling pump (RCP) during external power loss. We calculated the pressure by solving the nonlinear finite element equation composed of the linear Reynolds equation of an incompressible liquid lubricant and the nonlinear Reynolds equation of a compressible gas lubricant using the Newton–Raphson method. In addition, we calculated the temperature distribution by solving the two-dimensional energy equation utilizing the finite element method. Additionally, we included the turbulence effect in the incompressible liquid lubricant and the turbulence and slip effects in the compressible gas lubricant. The accuracy of the developed program was validated by comparing the simulated opening force and leakage rate of both the mechanical seal with the liquid lubricant and the mechanical seal with the gas lubricant with prior research. Our analysis shows that in high-temperature environments, the increase in the gas region at the lubrication surface leads to a decrease in pressure and opening force and an increase in the leakage rate. Conversely, as the outer pressure increases, the gas region decreases, resulting in an increase in pressure, opening force, and leakage rate. Full article
7 pages, 2589 KiB  
Article
Electromagnetic Modeling of Superconducting Bulks in Applied Time-Varying Magnetic Field
by Hocine Menana
Condens. Matter 2024, 9(4), 47; https://doi.org/10.3390/condmat9040047 - 9 Nov 2024
Viewed by 323
Abstract
An integrodifferential model formulated in terms of the electric vector potential is developed for the 3D numerical modeling of the electromagnetic field in superconducting bulks, for AC losses evaluation. The Newton Raphson method is applied to accelerate the convergence. The model is validated [...] Read more.
An integrodifferential model formulated in terms of the electric vector potential is developed for the 3D numerical modeling of the electromagnetic field in superconducting bulks, for AC losses evaluation. The Newton Raphson method is applied to accelerate the convergence. The model is validated on a benchmark. The comparison results show the accuracy of the model and its performances in terms of computation time compared to classical approaches. Full article
Show Figures

Figure 1

Figure 1
<p>HTS cube submitted to an external time-varying magnetic field.</p>
Full article ">Figure 2
<p>Instantaneous losses in the HTS cube.</p>
Full article ">Figure 3
<p>Eddy current distribution in the HTS cube, with magnitude normalized to <span class="html-italic">Jc</span>: (<b>a</b>) <span class="html-italic">t</span> = T/4 and (<b>b</b>) <span class="html-italic">t</span> = 3T/4.</p>
Full article ">Figure 4
<p>Eddy current distribution in the sub-cubes, with magnitudes normalized to <span class="html-italic">Jc</span>, at <span class="html-italic">t</span> = <span class="html-italic">T</span>/4, with and without considering their electromagnetic coupling.</p>
Full article ">Figure 5
<p>Instantaneous losses in the entire and subdivided cube with and without electromagnetic coupling between the sub-cubes.</p>
Full article ">
22 pages, 1273 KiB  
Article
Estimation of Lifetime Performance Index for Generalized Inverse Lindley Distribution Under Adaptive Progressive Type-II Censored Lifetime Test
by Shixiao Xiao, Xue Hu and Haiping Ren
Axioms 2024, 13(10), 727; https://doi.org/10.3390/axioms13100727 - 18 Oct 2024
Viewed by 519
Abstract
The lifetime performance index (LPI) is an important metric for evaluating product quality, and research on the statistical inference of the LPI is of great significance. This paper discusses both the classical and Bayesian estimations of the LPI under an adaptive progressive type-II [...] Read more.
The lifetime performance index (LPI) is an important metric for evaluating product quality, and research on the statistical inference of the LPI is of great significance. This paper discusses both the classical and Bayesian estimations of the LPI under an adaptive progressive type-II censored lifetime test, assuming that the product’s lifetime follows a generalized inverse Lindley distribution. At first, the maximum likelihood estimator of the LPI is derived, and the Newton–Raphson iterative method is adopted to solve the numerical solution due to the log-likelihood equations having no analytical solutions. If the exact distribution of the LPI is not available, then the asymptotic confidence interval and bootstrap confidence interval of the LPI are constructed. For the Bayesian estimation, the Bayesian estimators of the LPI are derived under three different loss functions. Due to the complex multiple integrals involved in these estimators, the MCMC method is used to draw samples and further construct the HPD credible interval of the LPI. Finally, Monte Carlo simulations are used to observe the performance of these estimators in terms of the average bias and mean squared error, and two practical examples are used to illustrate the application of the proposed estimation method. Full article
Show Figures

Figure 1

Figure 1
<p>Schematic representation of the adaptive progressive type-II censored test.</p>
Full article ">Figure 2
<p>(<b>a</b>) The diagram of the PDF. (<b>b</b>) The diagram of the HF.</p>
Full article ">Figure 3
<p>(<b>a</b>) Fitting of GILD on duration of remission. (<b>b</b>) Fitting of GILD on failure time.</p>
Full article ">Figure 4
<p>The partial derivatives of the log-likelihood function.</p>
Full article ">
18 pages, 2623 KiB  
Article
Design and Applicability of Two-Step Fractional Newton–Raphson Method
by Naseem Zulfiqar Ali, Awais Gul Khan, Muhammad Uzair Awan, Loredana Ciurdariu and Kamel Brahim
Fractal Fract. 2024, 8(10), 582; https://doi.org/10.3390/fractalfract8100582 - 2 Oct 2024
Viewed by 798
Abstract
Developing two-step fractional numerical methods for finding the solution of nonlinear equations is the main objective of this research article. In addition, we present a detailed study of convergence analysis for the methods that have been proposed. By comparing numerically, we can see [...] Read more.
Developing two-step fractional numerical methods for finding the solution of nonlinear equations is the main objective of this research article. In addition, we present a detailed study of convergence analysis for the methods that have been proposed. By comparing numerically, we can see that the proposed methods significantly improve convergence rate and accuracy. Additionally, we demonstrate how our main results can be applied to basins of attraction. Full article
(This article belongs to the Special Issue Fractional Systems, Integrals and Derivatives: Theory and Application)
Show Figures

Figure 1

Figure 1
<p>Comparison of 5 standard problems according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) TSFNRM1, (<b>c</b>) TSFNRM2.</p>
Full article ">Figure 2
<p>Iterations Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>=</mo> <msup> <mi>x</mi> <mn>3</mn> </msup> <mo>−</mo> <mn>10</mn> </mrow> </semantics></math> with respect to FNM, TSFNRM1, and TSFNRM2.</p>
Full article ">Figure 3
<p>Comparison of 5 standard problems according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) TSFNRM1, (<b>c</b>) TSFNRM2.</p>
Full article ">Figure 4
<p>Iterations Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>=</mo> <msup> <mo form="prefix">sin</mo> <mn>2</mn> </msup> <mi>x</mi> <mo>−</mo> <msup> <mi>x</mi> <mn>2</mn> </msup> <mo>+</mo> <mn>1</mn> </mrow> </semantics></math> with respect to FNM, TSFNRM1, and TSFNRM2.</p>
Full article ">Figure 5
<p>Comparison of 5 problems according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) TSFNRM1, (<b>c</b>) TSFNRM2.</p>
Full article ">Figure 6
<p>Iterations Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>=</mo> <msqrt> <mrow> <msup> <mi>x</mi> <mn>2</mn> </msup> <mo>+</mo> <mn>2</mn> <mi>x</mi> <mo>+</mo> <mn>5</mn> </mrow> </msqrt> <mo>−</mo> <mn>2</mn> <mo form="prefix">sin</mo> <mi>x</mi> <mo>−</mo> <msup> <mi>x</mi> <mn>2</mn> </msup> <mo>+</mo> <mn>3</mn> </mrow> </semantics></math> with respect to FNM, TSFNRM1, and TSFNRM2.</p>
Full article ">Figure 7
<p>Comparison of 5 standard problems according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) TSFNRM1, (<b>c</b>) TSFNRM2.</p>
Full article ">Figure 8
<p>Iterations Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>4</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>=</mo> <msup> <mi>x</mi> <mn>3</mn> </msup> <mo>+</mo> <mn>3</mn> <msup> <mi>x</mi> <mn>2</mn> </msup> <mo>+</mo> <mi>x</mi> <mo>−</mo> <mn>2</mn> </mrow> </semantics></math> with respect to FNM, TSFNRM1, and TSFNRM2.</p>
Full article ">Figure 9
<p>Comparison of 5 standard problems according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) TSFNRM1, (<b>c</b>) TSFNRM2.</p>
Full article ">Figure 10
<p>Iterations Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>5</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> <mo>=</mo> <msup> <mi>e</mi> <mrow> <mo>−</mo> <mi>x</mi> </mrow> </msup> <mo>+</mo> <mo form="prefix">cos</mo> <mi>x</mi> </mrow> </semantics></math> with respect to FNM, TSFNRM1, and TSFNRM2.</p>
Full article ">Figure 11
<p>Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>3</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) PIM4, (<b>c</b>) PIM5.</p>
Full article ">Figure 12
<p>Comparison of <math display="inline"><semantics> <mrow> <msub> <mi>f</mi> <mn>5</mn> </msub> <mrow> <mo>(</mo> <mi>x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> according to residual logarithm per iteration of (<b>a</b>) FNM, (<b>b</b>) PIM4, (<b>c</b>) PIM5.</p>
Full article ">Figure 13
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>1</mn> </msub> </semantics></math> by using FNM at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 14
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>1</mn> </msub> </semantics></math> by using TSFNRM2 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 15
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>1</mn> </msub> </semantics></math> by using TSFNRM1 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 16
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>2</mn> </msub> </semantics></math> by using FNM at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 17
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>2</mn> </msub> </semantics></math> by using TSFNRM2 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 18
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>2</mn> </msub> </semantics></math> by using TSFNRM1 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 19
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>3</mn> </msub> </semantics></math> by using FNM at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.3</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 20
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>3</mn> </msub> </semantics></math> by using TSFNRM1 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.3</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 21
<p>Basin of attraction for <math display="inline"><semantics> <msub> <mi>P</mi> <mn>3</mn> </msub> </semantics></math> by using TSFNRM2 at (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.3</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.7</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <mn>0.9</mn> </mrow> </semantics></math>.</p>
Full article ">
19 pages, 15139 KiB  
Article
Ultra-Short-Term Photovoltaic Power Prediction by NRGA-BiLSTM Considering Seasonality and Periodicity of Data
by Hong Wu, Haipeng Liu, Huaiping Jin and Yanping He
Energies 2024, 17(18), 4739; https://doi.org/10.3390/en17184739 - 23 Sep 2024
Cited by 1 | Viewed by 851
Abstract
Photovoltaic (PV) power generation is highly stochastic and intermittent, which poses a challenge to the planning and operation of existing power systems. To enhance the accuracy of PV power prediction and ensure the safe operation of the power system, a novel approach based [...] Read more.
Photovoltaic (PV) power generation is highly stochastic and intermittent, which poses a challenge to the planning and operation of existing power systems. To enhance the accuracy of PV power prediction and ensure the safe operation of the power system, a novel approach based on seasonal division and a periodic attention mechanism (PAM) for PV power prediction is proposed. First, the dataset is divided into three components of trend, period, and residual under fuzzy c-means clustering (FCM) and the seasonal decomposition (SD) method according to four seasons. Three independent bidirectional long short-term memory (BiLTSM) networks are constructed for these subsequences. Then, the network is optimized using the improved Newton–Raphson genetic algorithm (NRGA), and the innovative PAM is added to focus on the periodic characteristics of the data. Finally, the results of each component are summarized to obtain the final prediction results. A case study of the Australian DKASC Alice Spring PV power plant dataset demonstrates the performance of the proposed approach. Compared with other paper models, the MAE, RMSE, and MAPE performance evaluation indexes show that the proposed approach has excellent performance in predicting output power accuracy and stability. Full article
(This article belongs to the Section A2: Solar Energy and Photovoltaic Systems)
Show Figures

Figure 1

Figure 1
<p>Framework of the proposed model.</p>
Full article ">Figure 2
<p>PV active power profile of DKASC.</p>
Full article ">Figure 3
<p>Heat map of Pearson coefficient results.</p>
Full article ">Figure 4
<p>Sequence of characteristics of different seasons after seasonal division (<b>a</b>) spring, (<b>b</b>) summer, (<b>c</b>) autumn, (<b>d</b>) winter.</p>
Full article ">Figure 5
<p>The decomposition results of spring feature F0. (<b>a</b>) Trend component, (<b>b</b>) period component, (<b>c</b>) residual component.</p>
Full article ">Figure 6
<p>Predictive effectiveness of each model under different algorithms.</p>
Full article ">
28 pages, 563 KiB  
Article
Exploring a Dynamic Homotopy Technique to Enhance the Convergence of Classical Power Flow Iterative Solvers in Ill-Conditioned Power System Models
by Alisson Lima-Silva and Francisco Damasceno Freitas
Energies 2024, 17(18), 4642; https://doi.org/10.3390/en17184642 - 17 Sep 2024
Viewed by 626
Abstract
This paper presents a dynamic homotopy technique that can be used to calculate a preliminary result for a power flow problem (PFP). This result can then be used as an initial estimate to efficiently solve the PFP using either the classical Newton-Raphson (NR) [...] Read more.
This paper presents a dynamic homotopy technique that can be used to calculate a preliminary result for a power flow problem (PFP). This result can then be used as an initial estimate to efficiently solve the PFP using either the classical Newton-Raphson (NR) method or its fast decoupled version (FDXB) while still maintaining high accuracy. The preliminary stage for the dynamic homotopy problem is formulated and solved by employing integration techniques, where implicit and explicit schemes are studied. The dynamic problem assumes an initial condition that coincides with the initial estimate for a traditional iterative method such as NR. In this sense, the initial guess for the FPF is adequately set as a flat start, which is a starting for the case when this initialization is of difficult assignment for convergence. The static homotopy method requires a complete solution of a PFP per homotopy pathway point, while the dynamic homotopy is based on numerical integration methods. This approach can require only one LU factorization at each point of the pathway. Allocating these points properly helps avoid several PFP resolutions to build the pathway. The hybrid technique was evaluated for large-scale systems with poor conditioning, such as a 109,272-bus model and other test systems under stressed conditions. A scheme based on the implicit backward Euler scheme demonstrated the best performance among other numerical solvers studied. It provided reliable partial results for the dynamic homotopy problem, which proved to be suitable for achieving fast and highly accurate solutions using both the NR and FDXB solvers. Full article
(This article belongs to the Special Issue Modeling, Simulation and Optimization of Power System)
Show Figures

Figure 1

Figure 1
<p>Results determined by using only NR and a combination of dynamic homotopy, with <math display="inline"><semantics> <mrow> <mo>Δ</mo> <mi>t</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, and the NR solver.</p>
Full article ">Figure 2
<p>Integration solver performance when a smaller time-step <math display="inline"><semantics> <mrow> <mo>Δ</mo> <mi>t</mi> <mo>=</mo> <mn>0.125</mn> </mrow> </semantics></math> was adopted after the step <math display="inline"><semantics> <mrow> <msub> <mi>t</mi> <mn>1</mn> </msub> <mo>=</mo> <mn>0.01</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 3
<p>Plots indicating the evolution of the infinite norm of the PFP mismatches for three test systems when the NR solver is initialized by an explicit (FE or RK2) or implicit (BE) integration scheme, considering the homotopy pathway with five points, but only the instant <math display="inline"><semantics> <msub> <mi>t</mi> <mn>3</mn> </msub> </semantics></math> is changed.</p>
Full article ">Figure 4
<p>Results for the evolution of states and decaying power mismatches for the <tt>case109272</tt>, when the BE solver is used for the dynamic homotopy process and the results are refined by the NR solver.</p>
Full article ">Figure 5
<p>Evolution of the voltage magnitude and phase angle with the index <span class="html-italic">k</span> of a time instant <math display="inline"><semantics> <msub> <mi>t</mi> <mi>k</mi> </msub> </semantics></math> of the dynamic homotopy solver BE (dotted lines) or iterations for the NR solver (solid lines). Results are for the bus #6 of <tt>case109272</tt>, with different <math display="inline"><semantics> <mrow> <mo>Δ</mo> <mi>t</mi> </mrow> </semantics></math>.</p>
Full article ">
31 pages, 18202 KiB  
Article
MATLAB Application for Determination of 12 Combustion Products, Adiabatic Temperature and Laminar Burning Velocity: Development, Coding and Explanation
by Roberto Franco Cisneros and Freddy Jesus Rojas
Computation 2024, 12(9), 189; https://doi.org/10.3390/computation12090189 - 16 Sep 2024
Cited by 1 | Viewed by 653
Abstract
The determination of the characteristics and main combustion properties of fuels is necessary for post-implementation in different applications. Among the most important combustion properties of a fuel are the combustion products, flame temperature and laminar burning velocity. Therefore, this paper describes the step-by-step [...] Read more.
The determination of the characteristics and main combustion properties of fuels is necessary for post-implementation in different applications. Among the most important combustion properties of a fuel are the combustion products, flame temperature and laminar burning velocity. Therefore, this paper describes the step-by-step development and coding of a MATLAB application that can determine 12 combustion products, flame temperature and laminar burning velocity in order to understand the logic of calculus procedure, so any user would be able to make improvements of new functionalities (add more fuels, add more combustion products, etc.). The numerical procedure and methods (Gaussian elimination, Taylor Series and Newton–Raphson) parallel with their implementation as code lines for the development of the application are carried out using flow charts. In addition, simulations in Ansys Chemkin were performed and included in the application as part of the results comparison. It was found that: (1) The MATLAB Application codification and development were successfully explained in detail, (2) the functions and execution sequence are described by using flow charts and code extract, (3) the application is available to everyone for modifications, (4) the application can only be used for hydrocarbons fuels, (5) the application execution time registered was less than 8 s. Full article
Show Figures

Figure 1

Figure 1
<p>Methodology for the present work.</p>
Full article ">Figure 2
<p>Initial verification of fuel ID and lecture of properties in New_code.m: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 3
<p>Determination of the fuel enthalpy in New_code.m: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 3 Cont.
<p>Determination of the fuel enthalpy in New_code.m: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 4
<p>Determination of the air enthalpy and whole reactants enthalpy: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 5
<p>Definition of the activation energy, first estimate temperature, pressure and variables for the iteration process: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 6
<p>Iteration process for the determination of the product fractions, flame temperature and laminar burning velocity: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 7
<p>First definitions and verification of the initial defined estimated temperature: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 8
<p>Definition and determination of constants and verification of the equivalent ratio: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 9
<p>Definition of the equilibrium constants at constant pressure (Kp): (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 10
<p>First estimation of ‘PAR’ (X13), the definition of ‘df’ and ‘ox’ variables for Newton–Raphson iteration process: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 10 Cont.
<p>First estimation of ‘PAR’ (X13), the definition of ‘df’ and ‘ox’ variables for Newton–Raphson iteration process: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 11
<p>Newton–Raphson method: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 11 Cont.
<p>Newton–Raphson method: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 12
<p>Definition of equations for the other combustion products and their derivatives for matrix equation system: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 13
<p>Resolution of the matrix equation system by Gaussian elimination method using row interchange: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 14
<p>Final verification of the existence of a singular matrix in the matrix system: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 15
<p>Verification of the results tolerance and final calculation of the products: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 16
<p>Recalculation of variables for post operations procedure: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 17
<p>Introduction of properties and products data to the program: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 18
<p>Definition of derivatives respect temperature, pressure and ratio: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 19
<p>Resolution of the matrix equation system by Gaussian elimination method using maximum pivot strategy: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 20
<p>Verification of the existence of a singular matrix in the system: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 20 Cont.
<p>Verification of the existence of a singular matrix in the system: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 21
<p>Recalculation of partial derivatives: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 22
<p>Determination of the single row matrix SH: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 23
<p>Determination of average molar mass (AVM) and products enthalpy: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 24
<p>Determination of CP and partial derivative of enthalpy respect temperature: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 25
<p>Properties definition in the application: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 26
<p>Definition of molar fraction list items: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 27
<p>Definition of the fuel list and lecture of the Ansys Chemkin simulations results: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 28
<p>Setting of the variables for plotting: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 29
<p>MATLAB and plot functions: (<b>a</b>) Code line, (<b>b</b>) Flowchart.</p>
Full article ">Figure 30
<p>Application first screen with identified tools [<a href="#B8-computation-12-00189" class="html-bibr">8</a>].</p>
Full article ">Figure 31
<p>Results comparison with references [<a href="#B11-computation-12-00189" class="html-bibr">11</a>,<a href="#B12-computation-12-00189" class="html-bibr">12</a>] for Methane: (<b>a</b>) Flame temperature (K) versus equivalence ratio, (<b>b</b>) Laminar burning velocity (cm/s) versus equivalence ratio.</p>
Full article ">Figure 32
<p>Results comparison for Propane: (<b>a</b>) Flame temperature (K) versus equivalence ratio, (<b>b</b>) Laminar burning velocity versus equivalence ratio compared with references [<a href="#B13-computation-12-00189" class="html-bibr">13</a>,<a href="#B14-computation-12-00189" class="html-bibr">14</a>].</p>
Full article ">Figure 33
<p>Results comparison with research referenced as [<a href="#B15-computation-12-00189" class="html-bibr">15</a>] for different compositions of Natural Gas Laminar burning velocity versus equivalence ratio.</p>
Full article ">Figure A1
<p>New_code.m flowchart.</p>
Full article ">Figure A2
<p>Fractions_derivatives flowchart: (<b>a</b>) Part 1, (<b>b</b>), Part 2, (<b>c</b>) Part 3, (<b>d</b>) Part 4, (<b>e</b>) Part 5.</p>
Full article ">Figure A2 Cont.
<p>Fractions_derivatives flowchart: (<b>a</b>) Part 1, (<b>b</b>), Part 2, (<b>c</b>) Part 3, (<b>d</b>) Part 4, (<b>e</b>) Part 5.</p>
Full article ">Figure A2 Cont.
<p>Fractions_derivatives flowchart: (<b>a</b>) Part 1, (<b>b</b>), Part 2, (<b>c</b>) Part 3, (<b>d</b>) Part 4, (<b>e</b>) Part 5.</p>
Full article ">Figure A2 Cont.
<p>Fractions_derivatives flowchart: (<b>a</b>) Part 1, (<b>b</b>), Part 2, (<b>c</b>) Part 3, (<b>d</b>) Part 4, (<b>e</b>) Part 5.</p>
Full article ">Figure A2 Cont.
<p>Fractions_derivatives flowchart: (<b>a</b>) Part 1, (<b>b</b>), Part 2, (<b>c</b>) Part 3, (<b>d</b>) Part 4, (<b>e</b>) Part 5.</p>
Full article ">Figure A3
<p>MATLAB_Application.mlapp initialize flowchart.</p>
Full article ">
14 pages, 1181 KiB  
Article
Prediction of Wind Turbine Gearbox Oil Temperature Based on Stochastic Differential Equation Modeling
by Hongsheng Su, Zonghao Ding and Xingsheng Wang
Mathematics 2024, 12(17), 2783; https://doi.org/10.3390/math12172783 - 9 Sep 2024
Viewed by 503
Abstract
Aiming at the problem of high failure rate and inconvenient maintenance of wind turbine gearboxes, this paper establishes a stochastic differential equation model that can be used to fit the change of gearbox oil temperature and adopts an iterative computational method and Markov-based [...] Read more.
Aiming at the problem of high failure rate and inconvenient maintenance of wind turbine gearboxes, this paper establishes a stochastic differential equation model that can be used to fit the change of gearbox oil temperature and adopts an iterative computational method and Markov-based modified optimization to fit the prediction sequence in order to realize the accurate prediction of gearbox oil temperature. The model divides the oil temperature change of the gearbox into two parts, internal aging and external random perturbation, adopts the approximation theorem to establish the internal aging model, and uses Brownian motion to simulate the external random perturbation. The model parameters were calculated by the Newton–Raphson iterative method based on the gearbox oil temperature monitoring data. Iterative calculations and Markov-based corrections were performed on the model prediction data. The gearbox oil temperature variations were simulated in MATLAB, and the fitting and testing errors were calculated before and after the iterations. By comparing the fitting and testing errors with the ordinary differential equations and the stochastic differential equations before iteration, the iterated model can better reflect the gear oil temperature trend and predict the oil temperature at a specific time. The accuracy of the iterated model in terms of fitting and prediction is important for the development of preventive maintenance. Full article
Show Figures

Figure 1

Figure 1
<p>Comparison of gearbox oil temperature monitoring data with predicted values from stochastic differential equation models.</p>
Full article ">Figure 2
<p>Relative error plot for stochastic differential equation model of gearbox oil temperature.</p>
Full article ">Figure 3
<p>Comparison of gearbox oil temperature monitoring data with the predicted values of the ordinary differential equation model.</p>
Full article ">Figure 4
<p>Plot of fitting error change.</p>
Full article ">Figure 5
<p>Plot of test error variation.</p>
Full article ">
14 pages, 3954 KiB  
Article
Test Method for Single Satellite’s Inter-Satellite Link Pointing and Tracking via Ground Station
by Zhenqiang Hong, Xuxing Huang, Lifeng Yang, Zhiqiang Bian, Yong Yang and Shuang Li
Aerospace 2024, 11(9), 713; https://doi.org/10.3390/aerospace11090713 - 31 Aug 2024
Viewed by 682
Abstract
An inter-satellite link is a key technology that improves control accuracy, transmission efficiency, and autonomous capability of constellations. A satellite’s pointing and tracking abilities mainly determine the inter-satellite link’s performance, which should be validated through an in-orbit test. However, during the construction of [...] Read more.
An inter-satellite link is a key technology that improves control accuracy, transmission efficiency, and autonomous capability of constellations. A satellite’s pointing and tracking abilities mainly determine the inter-satellite link’s performance, which should be validated through an in-orbit test. However, during the construction of the constellation, the distribution of satellites does not satisfy the constraints of establishing the inter-satellite link. A test method for inter-satellite link pointing and tracking is developed with respect to a single satellite. A practical mission scenario for testing inter-satellite links’ performance is constructed. A virtual satellite is introduced as the target satellite to establish an inter-satellite link with the local satellite. The orbit of the virtual target satellite between two ground stations is characterized based on the Newton–Raphson method. By comparing the predicted and actual time differences between two ground stations receiving the signals from the local satellite, the inter-satellite link pointing and tracking abilities are evaluated independently. Numerical simulations verify the design of the virtual satellite. The single satellite test method for inter-satellite link pointing and tracking abilities is available. Full article
(This article belongs to the Special Issue Spacecraft Dynamics and Control (2nd Edition))
Show Figures

Figure 1

Figure 1
<p>Definition of the link beam pointing angle. <span class="html-italic">γ<sub>oa</sub></span> denotes the off-axis angle; <span class="html-italic">γ<sub>ra</sub></span> denotes the rotation angle.</p>
Full article ">Figure 2
<p>Indirect test process for single satellite’s inter-satellite links pointing and tracking.</p>
Full article ">Figure 3
<p>Test method for inter-satellite link pointing and tracking.</p>
Full article ">Figure 4
<p>Schematic diagram of the inter-satellite link between the two satellites in-orbit.</p>
Full article ">Figure 5
<p>Newton–Raphson method convergence curve of the time difference in the target satellite passing above ground stations A and B.</p>
Full article ">Figure 6
<p>Inter-satellite link pointing in the 3D scene.</p>
Full article ">Figure 7
<p>Ground projection of inter-satellite link of the local satellite.</p>
Full article ">Figure 8
<p>Signal reception time of ground stations during tracking of inter-satellite links.</p>
Full article ">Figure 9
<p>Inter-satellite link pointing to the off-axis angle (OA) and rotation angle (RA) curves.</p>
Full article ">
18 pages, 12471 KiB  
Article
Research on Prediction of Ash Content in Flotation-Recovered Clean Coal Based on NRBO-CNN-LSTM
by Yujiao Li, Haizeng Liu and Fucheng Lu
Minerals 2024, 14(9), 894; https://doi.org/10.3390/min14090894 - 30 Aug 2024
Viewed by 764
Abstract
Ash content is an important production indicator of flotation performance, reflecting the current operating conditions of the flotation system and the recovery rate of clean coal. It also holds significant importance for the intelligent control of flotation. In recent years, the development of [...] Read more.
Ash content is an important production indicator of flotation performance, reflecting the current operating conditions of the flotation system and the recovery rate of clean coal. It also holds significant importance for the intelligent control of flotation. In recent years, the development of machine vision and deep learning has made it possible to detect ash content in flotation-recovered clean coal. Therefore, a prediction method for ash content in flotation-recovered clean coal based on image processing of the surface characteristics of flotation froth is studied. A convolutional neural network –long short-term memory (CNN-LSTM) model optimized by Newton–Raphson is proposed for predicting the ash content of flotation froth. Initially, the collected flotation froth video is preprocessed to extract the feature dataset of flotation froth images. Subsequently, a hybrid CNN-LSTM network architecture is constructed. Convolutional neural networks are employed to extract image features, while long short-term memory networks capture time series information, enabling the prediction of ash content. Experimental results indicate that the prediction accuracy on the training set achieves an R value of 0.9958, mean squared error (MSE) of 0.0012, root mean square error (RMSE) of 0.0346, and mean absolute error (MAE) of 0.0251. On the test set, the prediction accuracy attains an R value of 0.9726, MSE of 0.0028, RMSE of 0.0530, and MAE of 0.0415. The proposed model effectively extracts flotation froth features and accurately predicts ash content. This study provides a new approach for the intelligent control of the flotation process and holds broad application prospects. Full article
Show Figures

Figure 1

Figure 1
<p>Coal flotation experimental equipment system diagram based on AI vision.</p>
Full article ">Figure 2
<p>Internal principle diagram of flotation cell.</p>
Full article ">Figure 3
<p>Comparison of flotation foam images before and after histogram equalization: (<b>a</b>) original image; (<b>b</b>) grayscale histogram of the original image; (<b>c</b>) image after histogram equalization; (<b>d</b>) grayscale histogram of the image after histogram equalization.</p>
Full article ">Figure 4
<p>Distribution of extracted bubble features per frame for each group. (<b>a</b>) Extraction of average bubble diameter per frame for each group; (<b>b</b>) extraction of bubble count per frame for each group; (<b>c</b>) extraction of rgb color per frame for each group; (<b>d</b>) extraction of hsi color per frame for each group; (<b>e</b>) extraction of the mean grayscale value of bubbles per frame for each group; (<b>f</b>) extraction of the skewness of bubbles per frame for each group; (<b>g</b>) extraction of each group’s bubble kurtosis per frame; (<b>h</b>) extraction of each group’s bubble median per frame; (<b>i</b>) extraction of bubble variance per frame for each group; (<b>j</b>) extraction of average bubble velocity per frame for each group.</p>
Full article ">Figure 4 Cont.
<p>Distribution of extracted bubble features per frame for each group. (<b>a</b>) Extraction of average bubble diameter per frame for each group; (<b>b</b>) extraction of bubble count per frame for each group; (<b>c</b>) extraction of rgb color per frame for each group; (<b>d</b>) extraction of hsi color per frame for each group; (<b>e</b>) extraction of the mean grayscale value of bubbles per frame for each group; (<b>f</b>) extraction of the skewness of bubbles per frame for each group; (<b>g</b>) extraction of each group’s bubble kurtosis per frame; (<b>h</b>) extraction of each group’s bubble median per frame; (<b>i</b>) extraction of bubble variance per frame for each group; (<b>j</b>) extraction of average bubble velocity per frame for each group.</p>
Full article ">Figure 5
<p>Coal flotation foam image of the dynamic characteristics of the light flow matching corresponding map points: (<b>a</b>) original graph feature point detection; (<b>b</b>) the feature points of adjacent frames are matched by optical flow.</p>
Full article ">Figure 6
<p>Flotation foam characteristic data convolution operation diagram. (<b>a</b>) 0 × 173 + 1 × 372 + 0 × 361 + 1 × 418 = 790. (<b>b</b>) 0 × 164.22 + 1 × 170.59 + 0 × 180.42 + 1 × 190.95 = 361.54. (<b>c</b>) 0 × 70.19 + 1 × 71.27 + 0 × 72.62 + 1 × 72.75 = 144.02. (<b>d</b>) 0 × 61.3 + 1 × 61.23 + 0 × 61.09 + 1 × 61.94 = 123.17.</p>
Full article ">Figure 7
<p>Flotation foam characteristic data pooling operation diagram.</p>
Full article ">Figure 8
<p>LSTM network structure diagram.</p>
Full article ">Figure 9
<p>CNN-LSTM composite network structure.</p>
Full article ">Figure 10
<p>Flotation foam training set predicted value and actual ash value training results.</p>
Full article ">Figure 11
<p>Flotation foam training set predicted value and actual ash value error diagram.</p>
Full article ">Figure 12
<p>Flotation foam test set predicted value and actual ash value training results.</p>
Full article ">Figure 13
<p>Flotation foam test set predicted value and actual ash value error diagram.</p>
Full article ">
22 pages, 1772 KiB  
Article
Optimal Searching-Based Reference Current Computation Algorithm for IPMSM Drives Considering Iron Loss
by Péter Stumpf and Tamás Tóth-Katona
Actuators 2024, 13(8), 321; https://doi.org/10.3390/act13080321 - 21 Aug 2024
Viewed by 636
Abstract
Interior permanent magnet synchronous machines (IPMSMs) are widely used as traction motors in the electric drive-train because of their high torque-per-ampere characteristics and potential for wide field weakening operation to expand the constant power range. The paper aims to introduce the most important [...] Read more.
Interior permanent magnet synchronous machines (IPMSMs) are widely used as traction motors in the electric drive-train because of their high torque-per-ampere characteristics and potential for wide field weakening operation to expand the constant power range. The paper aims to introduce the most important equations to calculate the operating trajectories of an IPMSM for optimal control. The main contribution is that the optimal operating trajectories are calculated by a feedforward, Newton–Raphson method-based searching algorithm that considers the iron loss resistance of IPMSMs. Steady-state calculations and dynamic simulation results prove the theoretical findings. Full article
(This article belongs to the Section High Torque/Power Density Actuators)
Show Figures

Figure 1

Figure 1
<p>A <math display="inline"> <semantics> <mrow> <mi>d</mi> <mi>q</mi> </mrow> </semantics> </math> axis equivalent circuit model of an IPMSM incorporating iron loss resistance; (<b>a</b>) <span class="html-italic">d</span> axis; (<b>b</b>) <span class="html-italic">q</span> axis.</p>
Full article ">Figure 2
<p>Operation regions of IPMSM on the <math display="inline"> <semantics> <mrow> <msub> <mi>i</mi> <mrow> <mi mathvariant="normal">d</mi> <mn>1</mn> </mrow> </msub> <mo>−</mo> <msub> <mi>i</mi> <mrow> <mi mathvariant="normal">q</mi> <mn>1</mn> </mrow> </msub> </mrow> </semantics> </math> plane.</p>
Full article ">Figure 3
<p>Block diagram of closed-loop control of the IPMSM.</p>
Full article ">Figure 4
<p>Flowchart of the operating mode selector assuming <math display="inline"> <semantics> <mrow> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mi mathvariant="normal">b</mi> </mrow> </msub> <mo>&lt;</mo> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mn>0</mn> </mrow> </msub> <mo>&lt;</mo> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mi>cr</mi> </mrow> </msub> </mrow> </semantics> </math>.</p>
Full article ">Figure 5
<p>Flowchart of the NR-based reference current calculation algorithm.</p>
Full article ">Figure 6
<p>Flowchart of the operating mode selector, assuming <math display="inline"> <semantics> <mrow> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mi mathvariant="normal">b</mi> </mrow> </msub> <mo>&lt;</mo> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mi>cr</mi> </mrow> </msub> <mo>&lt;</mo> <msub> <mo>Ω</mo> <mrow> <mi mathvariant="normal">m</mi> <mo>,</mo> <mn>0</mn> </mrow> </msub> </mrow> </semantics> </math>.</p>
Full article ">Figure 7
<p>Iterative convergence process of the NR-based reference current calculation algorithm for a working point given in the MTPA region (<math display="inline"> <semantics> <mrow> <msub> <mo>Ω</mo> <mi mathvariant="normal">m</mi> </msub> <mo>=</mo> <mn>150</mn> </mrow> </semantics> </math> rad/s, <math display="inline"> <semantics> <mrow> <msup> <mi>M</mi> <mo>*</mo> </msup> <mo>=</mo> <mn>10</mn> </mrow> </semantics> </math> Nm).</p>
Full article ">Figure 8
<p>Steady-state characteristic curves. (<b>a</b>) Numerically calculated <math display="inline"> <semantics> <mrow> <msubsup> <mi>i</mi> <mrow> <mi mathvariant="normal">d</mi> <mn>1</mn> </mrow> <mo>*</mo> </msubsup> <mo>−</mo> <msubsup> <mi>i</mi> <mrow> <mi mathvariant="normal">q</mi> <mn>1</mn> </mrow> <mo>*</mo> </msubsup> </mrow> </semantics> </math> trajectories at constant mechanical speeds; (<b>b</b>) maximum achievable electric torque (blue line) and allowable torque for continuous operation (dashed line) versus mechanical speed characteristics.</p>
Full article ">Figure 9
<p>Simulation results. Dynamic performance of the closed-loop current control using the proposed current reference generation algorithm with externally generated reference torque.</p>
Full article ">Figure 10
<p>Simulation results. Trajectory of the stator current in the <span class="html-italic">d</span>–<span class="html-italic">q</span> plane using the proposed current reference generation algorithm with externally generated reference torque.</p>
Full article ">Figure 11
<p>Simulation results. Dynamic performance of the closed-loop operation using the proposed current reference generation algorithm and utilizing an external speed controller.</p>
Full article ">
14 pages, 368 KiB  
Article
Fibonacci Wavelet Collocation Method for Solving Dengue Fever SIR Model
by Amit Kumar, Ayub Khan and Abdullah Abdullah
Mathematics 2024, 12(16), 2565; https://doi.org/10.3390/math12162565 - 20 Aug 2024
Viewed by 582
Abstract
The main focus in this manuscript is to find a numerical solution of a dengue fever disease model by using the Fibonacci wavelet method. The operational matrix of integration has been obtained using Fibonacci wavelets. The proposed method is called Fibonacci wavelet collocation [...] Read more.
The main focus in this manuscript is to find a numerical solution of a dengue fever disease model by using the Fibonacci wavelet method. The operational matrix of integration has been obtained using Fibonacci wavelets. The proposed method is called Fibonacci wavelet collocation method (FWCM). This biological model has been transformed into a system of nonlinear algebraic equations by using the Fibonacci wavelet collocation scheme. Afterward, this system has been solved by using the Newton–Raphson method. Finally, we provide evidence that our results are better than those obtained by various current approaches, both numerically and graphically, demonstrating the method’s accuracy and efficiency. Full article
Show Figures

Figure 1

Figure 1
<p>Comparison of solution <math display="inline"><semantics> <mrow> <mi>S</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">Figure 2
<p>Comparison of solution <math display="inline"><semantics> <mrow> <mi>I</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">Figure 3
<p>Comparison of solution <math display="inline"><semantics> <mrow> <mi>R</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">Figure 4
<p>Comparison and error plots for <math display="inline"><semantics> <mrow> <mi>S</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">Figure 5
<p>Comparison and error plots for <math display="inline"><semantics> <mrow> <mi>I</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">Figure 6
<p>Comparison and error plots for <math display="inline"><semantics> <mrow> <mi>R</mi> <mo>(</mo> <mi>t</mi> <mo>)</mo> </mrow> </semantics></math> vs. <span class="html-italic">t</span>.</p>
Full article ">
16 pages, 4713 KiB  
Article
An Efficient Quadratic Programming Method for Kinematic Control of Redundant Manipulators under Joint Velocity Constraints
by Zongdao Li, Pengfei Wang, Wenlong Zhao, Tao Wu and Qingdu Li
Actuators 2024, 13(7), 273; https://doi.org/10.3390/act13070273 - 20 Jul 2024
Viewed by 1125
Abstract
This paper presents an efficient inverse kinematics solution for redundant robotic arms. The proposed method combines the principles of continuation methods, improves the instability of the computation time by increasing the convergence of the kinematics function, and improves the efficiency of traditional numerical [...] Read more.
This paper presents an efficient inverse kinematics solution for redundant robotic arms. The proposed method combines the principles of continuation methods, improves the instability of the computation time by increasing the convergence of the kinematics function, and improves the efficiency of traditional numerical methods. The effectiveness and efficient performance of the method are demonstrated through comparative experiments. The computational speed of the method is twice as fast as the Newton–Raphson method under joint limit constraints and equal solution accuracy. Full article
(This article belongs to the Section Actuators for Robotics)
Show Figures

Figure 1

Figure 1
<p>Comparisons of IK problems using Diana7.</p>
Full article ">Figure 2
<p>Comparisons of IK problems using Kinova Gen3.</p>
Full article ">Figure 3
<p>Comparisons of IK problems using X02.</p>
Full article ">Figure 4
<p>Comparisons of IK problems using Kuka iiwa14.</p>
Full article ">Figure 5
<p>Comparisons of IK problems using Franka Emika Panda.</p>
Full article ">Figure 6
<p>Error convergence in iterations. CM1 and CM2 represent, respectively, the proposed method with different increments of the homotopy parameter <math display="inline"><semantics> <mrow> <mi mathvariant="sans-serif">Δ</mi> <mi>s</mi> </mrow> </semantics></math>.</p>
Full article ">Figure A1
<p>Agile robot Diana7 with the home configuration (in millimeters).</p>
Full article ">Figure A2
<p>X02 robot and its 7-DOF arms.</p>
Full article ">
18 pages, 3312 KiB  
Article
A Novel Geothermal Wellbore Model Based on the Drift-Flux Approach
by Yin Yuan, Weiqing Li, Jiawen Zhang, Junkai Lei, Xianghong Xu and Lihan Bian
Energies 2024, 17(14), 3569; https://doi.org/10.3390/en17143569 - 20 Jul 2024
Cited by 1 | Viewed by 786
Abstract
Geothermal energy, being a clean energy source, has immense potential, and accurate wellbore modeling is crucial for optimizing the drilling process and ensuring safety. This paper presents a novel geothermal wellbore model based on the drift-flux approach, tested under three different temperature and [...] Read more.
Geothermal energy, being a clean energy source, has immense potential, and accurate wellbore modeling is crucial for optimizing the drilling process and ensuring safety. This paper presents a novel geothermal wellbore model based on the drift-flux approach, tested under three different temperature and pressure well conditions. The proposed model integrates the conservation equations of mass, momentum, and energy, incorporating the gas–liquid two-phase flow drift-flux model and heat transfer model. The key features include handling the heat transfer between the formation and the wellbore, addressing the slip relationship between the gas and liquid phases, and accounting for wellbore friction. The nonlinear equations are discretized using the finite difference method, and the highly nonlinear system is solved using the Newton–Raphson method. The numerical simulation, validation, and comparison with existing models demonstrate the enhanced accuracy of this model. In our tests, the model achieved a high accuracy in calculating the bottom-hole pressure and temperature, with mean relative errors (MREs) significantly lower than those of other models. For example, the MREs for the bottom-hole pressure and temperature of the Rongxi area well in Xiongan, calculated by this model, are 1.491% and 1.323%, respectively. These results offer valuable insights for optimizing drilling parameters and ensuring drilling safety. Comparisons indicate that this approach significantly outperforms others in capturing the complex dynamics of geothermal wellbores, making it a superior tool for geothermal energy development. Full article
(This article belongs to the Section H2: Geothermal)
Show Figures

Figure 1

Figure 1
<p>Schematic of drilling circulation.</p>
Full article ">Figure 2
<p>Wellbore grid division.</p>
Full article ">Figure 3
<p>Xiongan Rongxi area well: (<b>a</b>) temperature results performance of different models; and (<b>b</b>) pressure results over time for different models.</p>
Full article ">Figure 4
<p>Comparison of the pressure–depth curves calculated by this model with the measured results.</p>
Full article ">Figure 5
<p>The pressure results calculated at different time points as a function of depth: (<b>a</b>) Akbar’s model; and (<b>b</b>) Tonkin’s model.</p>
Full article ">Figure 6
<p>SNLG87-29 well: (<b>a</b>) pressure vs. depth curve; and (<b>b</b>) temperature vs. depth curve.</p>
Full article ">Figure 7
<p>Well No. 6: (<b>a</b>) pressure vs. depth curve; and (<b>b</b>) temperature vs. depth curve.</p>
Full article ">
20 pages, 10916 KiB  
Article
Transient Friction Analysis of Pressure Waves Propagating in Power-Law Non-Newtonian Fluids
by Hang Li, Chenliang Ruan, Yanlin Su, Peng Jia, Haojia Wen and Xiuxing Zhu
Appl. Sci. 2024, 14(14), 6331; https://doi.org/10.3390/app14146331 - 20 Jul 2024
Viewed by 579
Abstract
Modulated pressure waves propagating in the drilling fluids inside the drill string are a reliable real-time communication technology that transmit data from downhole to the surface during oil and gas drilling. In the analysis of pressure waves’ propagation characteristics, the modeling of transient [...] Read more.
Modulated pressure waves propagating in the drilling fluids inside the drill string are a reliable real-time communication technology that transmit data from downhole to the surface during oil and gas drilling. In the analysis of pressure waves’ propagation characteristics, the modeling of transient friction in non-Newtonian fluids remains a great challenge. This paper establishes a numerical model for transient pipe flow of power-law non-Newtonian fluids by using the weighted residual collocation method. Then, the Newton–Raphson method is applied to solve the nonlinear equations. The numerical method is validated by using the theoretical solution of Newtonian fluids and is proven to converge reliably with larger time steps. Finally, the influencing factors of the wall shear stress are analyzed using this numerical method. For shear-thinning fluids, the friction loss of periodic flow decreases with the increase in flow rate, which is opposite to the variation law of friction with the flow rate for stable pipe flow. Keeping the amplitude of pressure pulsation unchanged, an increase in frequency leads to a decrease in velocity fluctuations; therefore, the friction loss decreases with the increase in frequency. Full article
Show Figures

Figure 1

Figure 1
<p>Pressure waves transmitted in drill string. (<b>a</b>) Fluid microelement segment used for pressure wave transmission analysis and flow parameters that do not vary radially. (<b>b</b>) Flow parameters of cylindrical microelement in transient friction analysis. The blue straight arrows represent the direction of liquid flow. The red curved arrows represent the propagation of pressure waves. The arrows in (<b>a</b>,<b>b</b>) represent the direction of forces.</p>
Full article ">Figure 2
<p>Numerical and analytical results for the startup flow of Newtonian fluids, where <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>t</mi> </mrow> <mrow> <mi>n</mi> </mrow> </msub> </mrow> </semantics></math> is the time for the numerical result and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>t</mi> </mrow> <mrow> <mi>a</mi> </mrow> </msub> </mrow> </semantics></math> is the time for the analytical result.</p>
Full article ">Figure 3
<p>Comparison of analytical and numerical results for startup flow under different power-law indexes <math display="inline"><semantics> <mrow> <mi>n</mi> </mrow> </semantics></math>. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.25</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.5</mn> </mrow> </semantics></math>, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.75</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 4
<p>Numerical and analytical results for the periodic flow of Newtonian fluids with different frequencies. The time of the curve shown in the figures is the last moment of a pulsating cycle.</p>
Full article ">Figure 5
<p>Comparison of analytical and numerical results for periodic flow with different frequency when power-law index <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>&lt;</mo> <mn>1</mn> </mrow> </semantics></math>; the time of the curve shown in the figures is the last moment of a pulsating cycle. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.6</mn> </mrow> </semantics></math> without correction, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.6</mn> </mrow> </semantics></math> after correction, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.85</mn> </mrow> </semantics></math> without correction, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.85</mn> </mrow> </semantics></math> after correction.</p>
Full article ">Figure 6
<p>Comparison of analytical and numerical results for periodic flow with different frequency when power-law index <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>&gt;</mo> <mn>1</mn> </mrow> </semantics></math>. The time of the curve shown in the figures is the last moment of a pulsating cycle. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.2</mn> </mrow> </semantics></math> without correction, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.2</mn> </mrow> </semantics></math> after correction, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.4</mn> </mrow> </semantics></math> without correction, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.4</mn> </mrow> </semantics></math> after correction.</p>
Full article ">Figure 6 Cont.
<p>Comparison of analytical and numerical results for periodic flow with different frequency when power-law index <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>&gt;</mo> <mn>1</mn> </mrow> </semantics></math>. The time of the curve shown in the figures is the last moment of a pulsating cycle. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.2</mn> </mrow> </semantics></math> without correction, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.2</mn> </mrow> </semantics></math> after correction, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.4</mn> </mrow> </semantics></math> without correction, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.4</mn> </mrow> </semantics></math> after correction.</p>
Full article ">Figure 7
<p><math display="inline"><semantics> <mrow> <mi>C</mi> <mfenced separators="|"> <mrow> <mi>n</mi> </mrow> </mfenced> </mrow> </semantics></math> varied with power-law index <math display="inline"><semantics> <mrow> <mi>n</mi> </mrow> </semantics></math>.</p>
Full article ">Figure 8
<p>Time history curve of velocity profile within half a cycle for different <math display="inline"><semantics> <mrow> <mi>n</mi> </mrow> </semantics></math>: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.75</mn> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.2</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 9
<p>Temporal and spatial distribution of shear stress. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>16</mn> <mi>π</mi> </mrow> </semantics></math> rad/s, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>32</mn> <mi>π</mi> </mrow> </semantics></math> rad/s.</p>
Full article ">Figure 10
<p>Temporal and spatial distribution of shear stress. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>16</mn> <mi>π</mi> </mrow> </semantics></math> rad/s, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.1</mn> </mrow> </semantics></math>; (<b>b</b>)<math display="inline"><semantics> <mrow> <mo> </mo> <mi>n</mi> <mo>=</mo> <mn>1</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>16</mn> <mi>π</mi> </mrow> </semantics></math> rad/s, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>; (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>16</mn> <mi>π</mi> </mrow> </semantics></math> rad/s, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.1</mn> </mrow> </semantics></math>; (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>ω</mi> <mo>=</mo> <mn>16</mn> <mi>π</mi> </mrow> </semantics></math> rad/s, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 11
<p>Variation of pulsating shear stress at the wall for different flow rate and ratio of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> to <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> </mrow> </semantics></math>. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math>. (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>1.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 12
<p>Variation of pulsating shear stress at the wall for different power-law indexes. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>Q</mi> <mo>=</mo> <mn>0.03</mn> <mo> </mo> <msup> <mrow> <mi mathvariant="normal">m</mi> </mrow> <mrow> <mn>3</mn> </mrow> </msup> <mo>/</mo> <mi mathvariant="normal">s</mi> </mrow> </semantics></math>; (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 13
<p>Variation of pulsating shear stress at the wall for different frequencies. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>Q</mi> <mo>=</mo> <mn>0.03</mn> <mo> </mo> <msup> <mrow> <mi mathvariant="normal">m</mi> </mrow> <mrow> <mn>3</mn> </mrow> </msup> <mo>/</mo> <mi mathvariant="normal">s</mi> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>p</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> <mn>0.2</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 14
<p>Relative pulsating shear stress at the wall varied with frequency.</p>
Full article ">
Back to TopTop