11 results about "Risk element" patented technology

The application discloses a water resource system risk multi-link conduction method, mainly comprising the following steps. Firstly, risk element data in a researched area are collected and standardized processing is conducted; then, water resource system risk links are constructed by using the correlation between risk elements; then, a risk conduction mechanism is defined: ①risk opening stage: simple mechanism of risk conduction and opening condition of risk are described; ②resistance threshold effect: the resistance ability of a system in risk conduction is described, according to the conduction characteristics of the risk link, the risk conduction mechanism and the resistance threshold effect of risk links with different structures are revealed; ③recovery threshold effect: natural and social repair forces make the risk not exist all the time, therefore, the risk recovery effect is defined; ④threshold value updating calculation: the resistance and recovery abilities are increased by risk prevention and control, therefore, the threshold value is updated; ⑤risk termination stage: the risk termination condition is deduced according to the risk conduction mechanism; ⑥risk intensity and conduction speed relationship: the greater the risk disturbance intensity is, the faster the risk conduction speed is. By exploring the risk link conduction mechanism, the water resource risk evaluation system under complex conditions is improved.

The invention discloses a low-altitude flight safety control method and device, computing equipment and a storage medium, the low-altitude flight safety control method is executed in the computing equipment, and the method comprises the following steps: based on a risk factor item, identifying a risk source existing in a flight task, the risk factor items comprise aircraft factors, personnel factors, environmental factors, airspace factors and management factors; calculating a risk score of each risk source by using a pre-constructed risk assessment model; the risk grade of the risk source is determined through the risk score, and the risk grade comprises high risk, medium risk or low risk; and selecting a corresponding flight strategy according to the risk level, and controlling the aircraft to execute the flight strategy. According to the method, the risk quantification model is constructed, a digital basis is provided for the feasibility of a flight task, and a powerful guarantee is provided for flight safety.

This invention discloses a method for runway landing event risk analysis based on association rules and complex networks, comprising the following steps: extracting risk factor keywords from runway landing accident investigation reports using Jieba word segmentation technology; constructing a runway landing event risk factor dataset based on the risk factor keywords; performing data mining processing on the runway landing event risk factor dataset using an association rule mining algorithm to obtain frequent itemsets and association rules; constructing a complex network based on frequent itemsets and association rules; the nodes of the complex network are frequent itemsets, and the edges of the complex network are the association rules; determining key risk nodes based on node degree and node centrality in the complex network, and marking them as key risk factors for runway landing events; and implementing prevention and control measures based on the key risk factors. This invention combines association rule mining and complex networks to analyze key risk factors for runway landing events and quantitatively calculates and analyzes the criticality of risk nodes.

This invention discloses a method, system, and medium for managing construction data during non-stop operation in the airfield, relating to the field of airport construction management. This invention introduces a dynamic Bayesian network model into airfield construction risk management. By dividing construction time slices and establishing temporal dependencies between risk factor nodes and target risk nodes, it achieves accurate modeling of the dynamic evolution of risks throughout the entire construction process. Utilizing diagnostic reasoning technology, it predicts the probability of occurrence of different risk factors at each construction stage and generates an intuitive risk distribution heatmap. This transforms risk management from traditional manual inspections, static assessments, and post-event responses into a new model of intelligent, dynamic prediction, and precise intervention, significantly improving the accuracy of risk identification, the timeliness of early warnings, and the effectiveness of management measures, fundamentally ensuring the safety and efficiency of airport operations during non-stop construction.

This invention provides a method and system for aviation emergency rescue risk assessment based on a large model, belonging to the field of aviation safety management technology. It addresses the limitations of existing technologies, such as strong subjectivity in assessment, insufficient multi-source data fusion analysis, and weak adaptability to extreme conditions. The method involves acquiring multi-source heterogeneous data associated with the flight to be assessed, fusing it to generate a standardized feature vector. This feature vector is then input into a pre-deployed risk assessment model, which is collaboratively constructed by a lightweight large model and a multi-factor dynamic fusion algorithm. The multi-factor dynamic fusion algorithm dynamically adjusts the weight coefficients of each risk factor based on real-time input, and then calls the lightweight large model to perform inference analysis on the correlation between risk factors, calculating the risk assessment result for the single flight. This invention significantly enhances the timeliness, safety, and overall effectiveness of rescue operations.

The invention belongs to the field of over-limit event risk analysis, and particularly discloses a flight training over-limit event relevance risk analysis method, system and device and a storage medium, and the method comprises the following steps: S1, pre-processing over-limit event data; s2, WGAN-GP data enhancement is carried out; s3, clustering interval division is carried out; and S4, correlation analysis and visualization are carried out. According to the invention, an improved WGAN-GP model is introduced to carry out data enhancement on flight features, and a training process is stabilized through a gradient penalty mechanism, so that the generated samples approach real data in distribution. According to the method, the variational Bayesian Gaussian mixture model is adopted to replace a traditional K-Means method, the optimal clustering number is automatically determined, and parameter interval label division is achieved. According to the method, mining results are constructed into a knowledge graph, structural expression among risk factors, flight states and overrun events is achieved, core risk nodes and key risk paths can be visually recognized through visual analysis, data analysis efficiency and result interpretability are greatly improved, and visual support is provided for flight safety decision making.

The specification provides a content security-oriented risk mining and answering method, device, medium and product. The content security-oriented risk mining method comprises: obtaining a question sample to be subjected to content security risk identification from at least one data source, and obtaining a plurality of risk elements from a preset security knowledge base; constructing a prompt word based on the question sample and the plurality of risk elements, and inputting the prompt word into a trained risk identification model to instruct the risk identification model to perform the following identification operation: identifying whether the question sample hits any of the plurality of risk elements; if not, performing content security risk analysis on the question sample to determine whether there is a new risk element; and if the risk identification model outputs a risk identification result that there is a new risk element, updating a risk identification process of an online answering system based on the new risk element in the risk identification result.

The application belongs to the technical field of data security, and discloses a risk element dynamic identification method and system based on a knowledge base updating mechanism, which comprises the following steps: formally describing a data cross-border flow business process, and extracting knowledge data involved in the business process; coding the knowledge data to form structured information, and storing the structured information into a knowledge base; performing step-by-step coding and concept refining on the structured information in the knowledge base, screening out a core category and other categories, and an association relationship between the core category and the other categories; and identifying risk elements in the data cross-border flow business process according to the association relationship. The application can realize continuous improvement and intelligent identification of data cross-border risk elements, thereby improving the completeness and accuracy of risk identification, and enhancing the overall efficiency of data cross-border security management.

The application discloses a kind of aircraft rush / cause runway event risk early warning and cause identification method and system, method includes: S0: by FOQA standard, SOP and QRH obtains the key parameter set and risk factor set of rush cause runway event;S1: based on the correspondence of key parameters and risk factors is constructed by Delphi method;S2: construct the rush cause runway risk prediction model based on Transformer, realize online risk identification;S3: based on hypothesis testing method obtains the most similar cause, completes risk factor identification.

The invention provides a risk assessment system and method for low-altitude flight based on a risk assessment model, and relates to the technical field of traffic management. The system comprises a model management module which is used for establishing a new risk assessment model according to a model name and an application service range, and managing the newly established risk assessment model and a historically established risk assessment model; the model configuration module is used for displaying a plurality of preset risk categories and risk factors thereof to the user based on the model name and the application service range, configuring a newly built risk assessment model according to the selection and / or input of the user, and sending the configured risk assessment model to the model management module; and the risk assessment module is used for acquiring a target risk assessment model selected by a user from the model management module according to the business type of the to-be-assessed flight application, and performing risk assessment on the to-be-assessed flight application based on the target risk assessment model, thereby realizing low-altitude flight risk assessment with good adaptability and good flexibility.

This disclosure provides a method for controlling a hoisting mechanism used to lift an aircraft in near space, comprising: setting the ultimate load that the aircraft must meet under target operating conditions based on risk factors that may cause abnormalities in the aircraft; establishing a finite element model to characterize the aircraft to be lifted and the hoisting mechanism used to lift the aircraft, and using the ultimate load as the excitation input of the finite element model to calculate the mechanical simulation under the target operating conditions to obtain displacement simulation data of the aircraft under the target operating conditions; manufacturing a solid scale-down model including the aircraft and the hoisting mechanism; adjusting the hoisting rope structure with the structural strength of the solid scale-down model of the aircraft as the limit, so that the solid scale-down model of the aircraft can switch between multiple target operating conditions, and constructing the allowable force envelope of each hoisting rope of the hoisting rope structure; controlling the hoisting mechanism carrying the aircraft based on the allowable force envelope of each hoisting rope, so that the aircraft can switch between multiple target operating conditions, from the lifting stage to the release stage.