optimal coefficient
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2021 ◽  
Vol ahead-of-print (ahead-of-print) ◽  
Author(s):  
Jiake Fu ◽  
Huijing Tian ◽  
Lingguang Song ◽  
Mingchao Li ◽  
Shuo Bai ◽  
...  

PurposeThis paper presents a new approach of productivity estimation of cutter suction dredger operation through data mining and learning from real-time big data.Design/methodology/approachThe paper used big data, data mining and machine learning techniques to extract features of cutter suction dredgers (CSD) for predicting its productivity. ElasticNet-SVR (Elastic Net-Support Vector Machine) method is used to filter the original monitoring data. Along with the actual working conditions of CSD, 15 features were selected. Then, a box plot was used to clean the corresponding data by filtering out outliers. Finally, four algorithms, namely SVR (Support Vector Regression), XGBoost (Extreme Gradient Boosting), LSTM (Long-Short Term Memory Network) and BP (Back Propagation) Neural Network, were used for modeling and testing.FindingsThe paper provided a comprehensive forecasting framework for productivity estimation including feature selection, data processing and model evaluation. The optimal coefficient of determination (R2) of four algorithms were all above 80.0%, indicating that the features selected were representative. Finally, the BP neural network model coupled with the SVR model was selected as the final model.Originality/valueMachine-learning algorithm incorporating domain expert judgments was used to select predictive features. The final optimal coefficient of determination (R2) of the coupled model of BP neural network and SVR is 87.6%, indicating that the method proposed in this paper is effective for CSD productivity estimation.


2020 ◽  
Vol 222 ◽  
pp. 03015
Author(s):  
Roman Beznosyuk ◽  
Dmitry Ryabchikov ◽  
Sergey Borychev ◽  
Georgiy Rembalovich ◽  
Mikhail Kostenko

For transporting potatoes, it is proposed to equip the vehicle with elastic partitions. Elastic partitions are formed by tubes of elastic material and can rotate around the axis of the transverse partition. A model has been developed that allows one to take into account a large number of parameters of root crops, a vehicle body, elastic partitions, parameters of the unloading process, and also calculate the main indicators of the efficiency of unloading root crops. As a result of optimization, it has been found that the optimal length of the elastic tube is 1.58 m (when the height of the vehicle body is 1.60 m), the optimal coefficient of bending stiffness of the tube is 0.9 kN/m2. At the same time, the unloading time will be less than 11.5 s and the share of damaged root crops will be less than 4.0%.


2018 ◽  
Vol 65 (5) ◽  
pp. 542-546 ◽  
Author(s):  
Sergio Callegari ◽  
Federico Bizzarri ◽  
Angelo Brambilla

2018 ◽  
Vol 0 (0) ◽  
pp. 0-0
Author(s):  
Seda İǧret Araz ◽  
◽  
Murat Subașı ◽  

2017 ◽  
Vol 140 (1) ◽  
Author(s):  
Ravon Venters ◽  
Brian T. Helenbrook ◽  
Kenneth D. Visser

This study presents a numerical optimization of a ducted wind turbine (DWT) to maximize power output. The cross section of the duct was an Eppler 423 airfoil, which is a cambered airfoil with a high lift coefficient (CL). The rotor was modeled as an actuator disk, and the Reynolds-averaged Navier–Stokes (RANS) k–ε model was used to simulate the flow. The optimization determined the optimal placement and angle for the duct relative to the rotor disk, as well as the optimal coefficient of thrust for the rotor. It was determined that the optimal coefficient of thrust is similar to an open rotor in spite of the fact that the local flow velocity is modified by the duct. The optimal angle of attack of the duct was much larger than the separation angle of attack of the airfoil in a freestream. Large angles of attack did not induce separation on the duct because the expansion caused by the rotor disk helped keep the flow attached. For the same rotor area, the power output of the largest DWT was 66% greater than an open rotor. For the same total cross-sectional area of the entire device, the DWT also outperformed an open rotor, exceeding Betz's limit by a small margin.


2016 ◽  
Vol 822 ◽  
pp. 389-396
Author(s):  
Laura Diana Grigorie ◽  
Alina Elena Romanescu ◽  
Daniela Vintilă

This paper presents mathematical models derived from the study of the chemical composition and mechanical properties of aluminum alloy type 6082 AlSi1MgMn. They were determined based on the study of the chemical composition of 30 batches of alloy 6082 and their mechanical properties. Mathematical models obtained were checked by Fisher test, and the two of them had the optimal coefficient of determination. Aluminum alloy was hot rolled and hardened through heat treatments.


2016 ◽  
Vol 2016 ◽  
pp. 1-14 ◽  
Author(s):  
Qingxuan Jia ◽  
Tong Li ◽  
Gang Chen ◽  
Hanxu Sun ◽  
Jian Zhang

Aiming at reducing joint velocity jumps caused by an unexpected joint-locked failure during space manipulator on-orbit operations without shutting down manipulator, trajectory optimization strategy considering the unexpectedness characteristics of joint-locked failure is proposed in the paper, which can achieve velocity jumps reduction in both operation space and joint space simultaneously. In the strategy, velocity in operation space concerning task completion directly is treated as equality constraints, and velocity in joint space concerning motion performance is treated as objective function. Global compensation vector which consists of coefficient, gradient of manipulability, and orthogonal matrix of null space is constructed to minimize the objective function. For each particular failure time, unique optimal coefficient can be obtained when the objective function is minimal. As a basis, a method for optimal coefficient function fitting is proposed based on a priori failure information (possible failure time and the corresponding optimal coefficient) to guarantee the unexpectedness characteristics of joint-locked failure. Simulations are implemented to validate the efficiency of trajectory optimization strategy in reducing velocity jumps in both joint space and operation space. And the feasibility of coefficient function is also verified in reducing velocity jump no matter when joint-locked failure occurs.


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