Probabilistic Hesitant Fuzzy Evidence Theory and Its Application in Capability Evaluation of a Satellite Communication System
<p>Indicator system construction process.</p> "> Figure 2
<p>Capability indicator system of SCS.</p> "> Figure 3
<p>Capability demand satisfaction evaluation process.</p> "> Figure 4
<p>Satisfaction degrees of different schemes.</p> "> Figure 5
<p>Stability analysis. (<b>a</b>) Fusion results with different indicator weights; (<b>b</b>) fusion results with different mission importance.</p> "> Figure 6
<p>Fusion results of different methods.</p> ">
Abstract
:1. Introduction
- We introduce the PHFBPA, which effectively represents information that is difficult to describe with exact values. The PHFBPA incorporates both membership degrees and probabilities, allowing for more ambiguous information representation. When the PHFBPA element is a single value, it degenerates to the basic probability assignment (BPA).
- The combination rule for PHFBPA based on the operators of PHFS and the decision-making strategy to make the final decision are proposed. A numerical example is provided to illustrate the feasibility of the combination rule.
- We develop two methods for generating PHFBPAs. The first method is based on the difference between actual and expected values, with the probability distribution of the element in the PHFE being determined by experts through system analysis. The second method is multi-classifier-based, where membership degrees and probabilities are obtained through training on a dataset.
- Discounting factors are designed to modify the PHFBPA. An entropy measure of PHFBPA is proposed as the credibility discounting factor, and its axiomatic properties are proven. The Jousselme distance of PHFBPAs is used as the reliability discounting factor to measure conflict between evidence.
- We compare the PHFET method with several machine learning algorithms for the classification of some UCI data sets, and the results demonstrate the effectiveness of the PHFET method.
- A model for evaluating SCS capability demand satisfaction degree based on PHFET is provided, which involves establishing a capability indicator system through task decomposition and fusing data from different indicators using the PHFET method. Furthermore, we simulate a representative case digitally to analyze the stability of PHFET and compare it with some traditional methods, highlighting the robustness and superiority of the PHFET method.
2. Preliminaries
2.1. Dempster–Shafer Theory
2.2. Probabilistic Hesitant Fuzzy Set Theory
2.3. Jousselme Distance
3. Probabilistic Hesitant Fuzzy Evidence Theory
3.1. The Concept of the Probabilistic Hesitant Fuzzy Evidence Theory
3.2. Generation Methods of Probabilistic Hesitant Fuzzy Basic Probability Assignment
3.2.1. Distance-Based Generation Method
- Step 1: Define the ideal values for each class. The ideal value of class i is denoted as , where is the ideal value of attribute . These values can be determined based on expert analysis of the system or through the use of clustering algorithms such as KMeans. For test sample , if is equal to , then is considered to belong to class i.
- Step 2: Calculate the distance between the actual and expected values. To generate the probability assignment for test sample S, we employ the Euclidean distance metric to quantify the dissimilarity. The Euclidean distance between S and each center is computed as follows:
- Step 3: Generate BPAs. The proximity of to a center determines the likelihood of belonging to that class. As moves further away from a center, its likelihood of belonging to that class diminishes. Therefore, the following formula is given to calculate the BPAs of the kth attribute:
- Step 4: Add the corresponding probabilities to the BPAs. The probabilities are determined by experts, and they are added to the BPAs to obtain the PHFE containing a single value .
- Step 5: Select different criteria and repeat Steps 1–4. Experts may have difficulty determining the ideal value for a specific focal element due to uncertainty or variability in evaluation criteria. Thus, n ideal values are determined based on different evaluation criteria for class i. By performing the aforementioned Steps 1–4 n times, we can obtain multiple elements , which collectively form the PHFBPA of attribute k for class i:
3.2.2. Multi-Classifier-Based Generation Method
- Step 1: Divide the original data set into a training set and test set.
- Step 2: Construct multiple classifiers. Utilize the training data to create n distinct classifiers for each piece of evidence. These classifiers are denoted as classifier . The output of each classifier should consist of sets of real numbers in , representing the degree to which a sample belongs to different classes. The classifiers should be capable of providing the probability of each class to which a sample belongs, denoted as . The accuracy of a classifier, represented as , measures the proportion of correctly classified samples. It can be calculated using the following formula:
- Step 3: Generate PHFBPAs. The test set is inputted into the trained classifiers to obtain the output of each classifier. The corresponding probability based on the accuracy of each classifier is calculated as follows:Subsequently, the PHFBPAs can be obtained as shown below:
3.3. Discounting Factors
3.3.1. Uncertainty Measurement
- 1.
- ;
- 2.
- iff ;
- 3.
- iff ;
- 4.
- ;
- 5.
- , if or and .
- Since and , then , and . From , we know . Then, , yielding ; thus, .
- iff iff , then or , .
- iff iff iff .
- Since , then .
- If or and , then . Hence, , which implies .
3.3.2. Conflict Measurement
4. Capability Evaluation of a Satellite Communication System
4.1. Capability Indicator System Construction
- Step 1: Task analysis. The initial step involves the decomposition of mission tasks to identify the capabilities that are necessary to support these tasks. Given that mission tasks are diverse in nature, the capabilities required to accomplish them are also varied. Thus, by breaking down the core mission task T, we obtain independent and unique sub-tasks at different levels, denoted as
- Step 2: Capability analysis. The specific execution of an activity requires certain capabilities, creating a one-to-one or one-to-many mapping relationship between activities and capabilities, denoted as follows:
- Step 3: Indicator analysis. A capability is defined by one or more capability indicators , which are measurable capability attributes. We decompose the capabilities to obtain sub-capabilities, and this iterative decomposition process continues until we reach a set of basic measurable, operable, and understandable attributes, that is, technical and tactical indicators of the system.
4.2. Capability Demand Satisfaction Degree Evaluation
5. Verification and Application
5.1. Verification on Classification
- XGBoost classifiers with booster options of gbtree and gblinear.
- SVM classifiers with radial basis function kernel and linear kernel.
- RF classifiers with criterion options of gini and entropy.
- Multi-Layer Perceptron (MLP) classifiers with two hidden layers using either 10-10 or 20-10 nodes, and tansig activation function.
- LR classifiers with LBFGS and Stochastic Average Gradient (SAG) solver, respectively.
5.2. Application on Capability Demand Satisfaction Evaluation of SCS
5.3. Discussion
6. Conclusions
Author Contributions
Funding
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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Data Set | Attribute Type | Instances | Attributes | Class | Subject Area |
---|---|---|---|---|---|
Statlog | Categorical, Integer, Real | 690 | 14 | 2 | Financial |
Breast Cancer | Real | 569 | 30 | 2 | Life |
Seeds | Real | 210 | 7 | 3 | Life |
CMSC | Real | 540 | 18 | 2 | Physical |
Heart disease | Categorical, Integer, Real | 303 | 13 | 5 | Life |
Wine | Integer, Real | 178 | 13 | 3 | Physical |
Ionosphere | Integer, Real | 351 | 34 | 2 | Physical |
Data Set | XGBoost-1 | XGBoost-2 | SVM-1 | SVM-2 | RF-1 | RF-2 | MLP-1 | MLP-2 | LR-1 | LR-2 | PHFET |
---|---|---|---|---|---|---|---|---|---|---|---|
Statlog | 0.8810 | 0.8578 | 0.8564 | 0.8534 | 0.8810 | 0.8883 | 0.8549 | 0.8549 | 0.8593 | 0.8593 | 0.8905 |
Breast cancer | 0.9701 | 0.9649 | 0.9210 | 0.9210 | 0.9649 | 0.9649 | 0.9139 | 0.8402 | 0.9438 | 0.9139 | 0.9912 |
Seeds | 0.9191 | 0.9571 | 0.9381 | 0.9429 | 0.9143 | 0.8952 | 0.9143 | 0.9000 | 0.9381 | 0.9381 | 0.9762 |
CMSC | 0.9204 | 0.9204 | 0.9204 | 0.9500 | 0.9500 | 0.9556 | 0.9574 | 0.9611 | 0.9630 | 0.9630 | 0.9630 |
Heart disease | 0.5710 | 0.5876 | 0.5808 | 0.5842 | 0.5841 | 0.5775 | 0.5940 | 0.6007 | 0.5875 | 0.5875 | 0.6333 |
Wine | 0.9492 | 0.9552 | 0.6571 | 0.9494 | 0.9776 | 0.9775 | 0.6356 | 0.6395 | 0.9494 | 0.7135 | 1.0000 |
Ionoshpere | 0.9345 | 0.8805 | 0.9402 | 0.8804 | 0.9402 | 0.9375 | 0.8719 | 0.8803 | 0.8803 | 0.8803 | 0.9486 |
Indicators | Demand Value of | Demand Value of | Demand Value of | Scheme 1 | Scheme 2 |
---|---|---|---|---|---|
0.9679 | 0.7364 | 0.6312 | 1 | 0.9772 | |
0.8878 | 0.6658 | 0.4439 | 0.9903 | 1 | |
1 | 0.9 | 0.7 | 0.9772 | 0.9897 | |
1 | 0.5 | 0.2 | 0.7789 | 0.8355 | |
0.9672 | 0.9188 | 0.8705 | 0.9636 | 1 | |
0.7921 | 0.9307 | 1 | 0.8267 | 0.8239 | |
0.1667 | 0.6667 | 1 | 0.3553 | 0.6927 | |
0.3333 | 0.5 | 1 | 0.4517 | 0.8553 | |
1 | 0.9333 | 0.8333 | 0.9719 | 0.9718 | |
0.8 | 0.8571 | 1 | 0.8083 | 0.8040 | |
1 | 0.8947 | 0.7895 | 0.9704 | 0.9742 | |
1 | 0.5 | 0.3125 | 0.9375 | 0.5000 |
Importance | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|
Land communication | 0.6 | 0.8 | 0.8 | 0.7 | 0.6 | 0.75 | 0.5 | 0.8 | 0.8 | 0.8 | 0.8 | 0.6 |
Maritime communication | 0.4 | 0.2 | 0.2 | 0.3 | 0.4 | 0.25 | 0.5 | 0.2 | 0.2 | 0.2 | 0.2 | 0.4 |
PHFBPAs | |||
---|---|---|---|
{0.3794(0.6), 0.3415(0.4)} | {0.3309(0.6), 0.2978(0.4)} | {0.2898(0.6), 0.26070(0.4)} | |
{0.4185(0.8), 0.3348(0.2)} | {0.3463(0.8), 0.2770(0.2)} | {0.2352(0.8), 0.18819(0.2)} | |
{0.3512(0.8), 0.2809(0.2)} | {0.3474(0.8), 0.2779(0.2)} | {0.3015(0.8), 0.2412(0.2)} | |
{0.3987(0.7), 0.2990(0.3)} | {0.3763(0.7), 0.2823(0.3)} | {0.2250(0.7), 0.1687(0.3)} | |
{0.3357(0.6), 0.2350(0.4)} | {0.3344(0.6), 0.2341(0.4)} | {0.3299(0.6), 0.2310(0.4)} | |
{0.3419(0.75),0.3248(0.25)} | {0.3354(0.75),0.3186(0.25)} | {0.3227(0.75),0.3066(0.25)} | |
{0.4251(0.5), 0.4039(0.5)} | {0.3761(0.5), 0.3573(0.5)} | {0.1988(0.5), 0.1889(0.5)} | |
{0.3865(0.8), 0.3092(0.2)} | {0.3956(0.8), 0.3165(0.2)} | {0.2179(0.8), 0.1743(0.2)} | |
{0.3376(0.8), 0.3038(0.2)} | {0.3371(0.8), 0.3034(0.2)} | {0.3254(0.8), 0.2928(0.2)} | |
{0.3419(0.8), 0.3761(0.2)} | {0.3403(0.8), 0.3744(0.2)} | {0.3177(0.8), 0.3495(0.2)} | |
{0.3415(0.8), 0.3073(0.2)} | {0.3382(0.8), 0.3044(0.2)} | {0.3204(0.8), 0.2884(0.2)} | |
{0.4654(0.6), 0.4189(0.4)} | {0.3199(0.6), 0.2879(0.4)} | {0.2147(0.8), 0.1933(0.4)} |
Weight Set | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 | 1/12 |
2 | 0.151 | 0.032 | 0.312 | 0.012 | 0.144 | 0.132 | 0.035 | 0.067 | 0.005 | 0.014 | 0.081 | 0.015 |
3 | 0.017 | 0.051 | 0.081 | 0.036 | 0.123 | 0.092 | 0.094 | 0.225 | 0.068 | 0.097 | 0.106 | 0.01 |
Importance Set | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|
2 | 0.96 | 0.52 | 0.7 | 0.32 | 0.27 | 0.4 | 0.67 | 0.18 | 0.63 | 0.73 | 0.68 | 0.54 |
0.04 | 0.48 | 0.3 | 0.68 | 0.73 | 0.6 | 0.33 | 0.82 | 0.37 | 0.27 | 0.32 | 0.46 | |
3 | 0.05 | 0.06 | 0.79 | 0.98 | 0.96 | 0.24 | 0.19 | 0.26 | 0.49 | 0.82 | 0.25 | 0.39 |
0.95 | 0.94 | 0.21 | 0.02 | 0.04 | 0.76 | 0.81 | 0.74 | 0.51 | 0.18 | 0.75 | 0.61 |
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Liu, J.; Jian, P.; Liu, D.; Xiong, W. Probabilistic Hesitant Fuzzy Evidence Theory and Its Application in Capability Evaluation of a Satellite Communication System. Entropy 2024, 26, 94. https://doi.org/10.3390/e26010094
Liu J, Jian P, Liu D, Xiong W. Probabilistic Hesitant Fuzzy Evidence Theory and Its Application in Capability Evaluation of a Satellite Communication System. Entropy. 2024; 26(1):94. https://doi.org/10.3390/e26010094
Chicago/Turabian StyleLiu, Jiahuan, Ping Jian, Desheng Liu, and Wei Xiong. 2024. "Probabilistic Hesitant Fuzzy Evidence Theory and Its Application in Capability Evaluation of a Satellite Communication System" Entropy 26, no. 1: 94. https://doi.org/10.3390/e26010094