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572 results about "Kinetic analysis" patented technology

Blood vessel of brain circulation kinetic analysis method and apparatus

The invention relates to a brain vascular blood circulation dynamic analysis method and the apparatus thereof. According to the cerebral circulation vascular bed anatomical model, an equivalent network model which comprises 12 pipeline units simulating the brain circulation blood dynamics is built, and the relevant parameter calculation formulas are confirmed, by utilizing the formulas, the flow rate waveform and the value inside the cartid artery, the pressure waveform, the blood pressure of the body, the diameter of the blood vessel, the flow rate waveform and the valve of the vertebral artery and the front, the middle and the rear parts on two sides inside the skull, and the characteristic and the parameter of the cartid artery and each blood vessel section inside the skull can be determined, the apparatus designed by the invention can be performed, the detecting system comprises the vessel diameter detecting of the cartid artery outside the skull, the blood pressure detecting, theblood flow rate detecting of the cartid artery outside the skull, the pressure waveform detecting of the cartid artery outside the skull, and the blood flow rate detecting on the artery inside the skull; the control system comprises a control module and a power supply module; the calculation and analysis system comprises a host computer, a peripheral equipment, and an analog-digital converter, the invention can fully analyze the brain circulation dynamic characteristic, thereby having notable effect on the early stage and the ultra early stage diagnosis and therapy of the brain vascular illness.
Owner:SHANGHAI KUANGFU MEDICAL EQUIP DEV

Dynamics performance parameter optimizing method of high-speed train

The invention provides a dynamics performance parameter optimizing method of a high-speed train, relates to the field of parameter design optimizing based on the dynamics simulation analysis of the high-speed train, and aims at effectively replacing a dynamics simulation model of the high-speed train by a comprehensive target neural network agent model and combining the design analysis and the multi-target optimization algorithm of the high-speed train in the multi-disciplinary field to analyze and optimize the dynamics simulation approximation model of the high-speed train. The method specifically comprises the steps of building a multi-rigidity dynamics simulation model for the high-speed train; determining related important input/ output design spaces; selecting sampling strategy to obtain a design space sample set suitable for the dynamics performance analysis of the high-speed train; improving the generalization accuracy of the comprehensive target neural network by the bayesian regularization method; adjusting the number of nodes in a hidden layer to build the comprehensive target neural network agent network model of which the error is controlled to be within a certain of range; performing multi-target optimization through the intelligent differential evolution algorithm by using the improved comprehensive target neural network agent network model to obtain the optimized high-speed train design parameters. The method is mainly applied to the dynamics analysis and design optimization of the high-speed train.
Owner:成都天佑创软科技有限公司

Coaxial rigid rotor pneumatic elastic response method

The invention provides a coaxial rigid rotor coupling pneumatic elastic response analysis method, and belongs to a helicopter kinetic analysis technology. The method is characterized in that according to the operation and control characteristics of a coaxial rigid rotor helicopter, a balance equation optimization solution method is built, and an optimization solution is found according to the given target and constraint conditions. According to the characteristic of complicated coaxial rigid rotor flow field environment, a rotor flow field is calculated by using a computational fluid dynamic method based on an Euler/N-S equation; and then, the coupling pneumatic elastic response is calculated by using a computational fluid dynamic/computational structural dynamic loose coupling analysis method. The coaxial rigid rotor coupling pneumatic elastic analysis method has the advantage that when the analysis method is used, balance operation and control parameters, blade response, rotor loads and the like of the coaxial rigid rotor helicopter can be calculated. The method has good analysis precision and engineering applicability; the relying of the development process on the test can be reduced; and the design period and the development cost can be greatly reduced.
Owner:CHINA HELICOPTER RES & DEV INST

Modal synthesis dynamic modeling and analysis method for automobile driving axle system

ActiveCN105677980AFast Kinetic AnalysisRealize Kinetic AnalysisGeometric CADSustainable transportationElement modelCar driving
The invention relates to a modal synthesis dynamic modeling and analysis method for an automobile driving axle system. The method is characterized by comprising the steps that 1, a finite element model of all components of a driving axle is established, boundary nodes are defined according to the connecting relation between the components, a modal synthesis model of all the components is established, and a modal synthesis rigidity matrix and a mass matrix of all the components are obtained; 2, a connecting relation model of all the components is established; 3, the modal synthesis rigidity matrix and the mass matrix of all the components are assembled according to the connecting relation, a complete modal synthesis dynamic model of the driving axle system is established, and a rigidity matrix and a mass matrix of the driving axle system are obtained; 4, natural vibration frequency and a regular vibration mode of the dynamic model of the driving axle system are calculated, and a mode superposition method is adopted to calculate the dynamic response of the driving axle system under excitation of dynamic engaging force of gears of a main reducing gear. In the whole modeling process, high universality and calculating efficiency are achieved, and the method can be widely applied to dynamic analysis of a gear transmission system.
Owner:TSINGHUA UNIV +1

Polyhedron collision dynamics analysis method for the process of space manipulator grabbing non-cooperative target

The invention provides a polyhedron collision dynamics analysis method for the process of a space manipulator grabbing a non-cooperative target. The method comprises the following steps of (1) establishing a dynamical model of a space manipulator; (2) expressing the tail end of the space manipulator as a combination of multiple polyhedrons, and expressing the non-cooperative target as a polyhedron; conducting collision detection on the polyhedron expressing the non-cooperative target through the multiple polyhedrons expressing the tail end of the space manipulator, and detecting whether two different polyhedrons collide or not; if not, repeating the step (2), and if yes, detecting the collision intersection point of the two different polyhedrons; (3) solving collision force in the process of the space manipulator grabbing the non-cooperative target through a non-linear damping model according to the collision intersection point of the two different polyhedrons; and (4) substituting the collision force into a dynamical equation to obtain the collision response in the grabbing process. The polyhedron collision dynamics analysis method is reasonable in design, simple in implementation, high in analytical calculation fidelity and closer to the practical situation.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Bidirectional fluid-solid coupling three-dimensional numerical simulation method for high-speed pantograph

The invention discloses a bidirectional fluid-solid coupling three-dimensional numerical simulation method for a high-speed pantograph. The method comprises the following steps: firstly, constructinggeometric models of a fluid domain and a solid domain of the high-speed pantograph; secondly, according to the model constructed in the first step, conducting grid division on a pantograph fluid domain and a pantograph solid domain respectively; then setting material parameters, initial conditions and boundary conditions of a fluid domain and a solid domain; adding a pantograph fluid-solid coupling data exchange surface, and performing bidirectional fluid-solid coupling numerical analysis of the high-speed pantograph; and finally, obtaining a pantograph displacement cloud picture and a stresscloud picture according to a kinetic analysis result in the step 4, and obtaining an aerodynamic time-history curve of each part of the pantograph according to a hydrodynamic analysis result. On the basis of the bidirectional fluid-solid coupling theoretical model, the change of the operation posture of the pantograph under the aerodynamic force effect is considered, aerodynamic characteristic calculation and stress deformation research of the pantograph under the high-speed airflow effect are achieved through numerical simulation, and the nature of the aerodynamic characteristics of the pantograph can be reflected more objectively.
Owner:SOUTHWEST JIAOTONG UNIV

Position attitude control method of four-rotor unmanned aerial vehicle with unbalance loads

The invention relates to a position attitude control method of a four-rotor unmanned aerial vehicle with unbalance loads, and belongs to the technical field of control of unmanned aerial vehicles, which aims at solving the problem of the unmanned aerial vehicle failing to continue to stably run due to unknown center of gravity and uncertainty in installation position in the process of loading unbalanced load. The position attitude control method comprises the following steps of firstly, deriving a kinematics model and a dynamics model before and after the unbalance load is loaded on the four-rotor unmanned aerial vehicle by coordinate conversion and dynamics analysis; obtaining the measuring data of a sensor in the flight process, utilizing a Kalman filtering method to obtain the high-precision and non-lagging flight state, and distinguishing the approximate location of center of gravity by the flight states; designing a position attitude controller and a position controller of the four-rotor unmanned aerial vehicle, and improving the controller by compensating the rotation speed of a propeller, so as to offset the additional rotary movement and linear movement due to location change of center of gravity. The position attitude control method is suitable for estimating the location of the center of gravity in the takeoff and hovering process of the four-rotor unmanned aerial vehicle, and establishing a compensation controller.
Owner:HARBIN INST OF TECH

Cyanobacterial bloom predicting method based on non-linear kinetic time-series model

The invention discloses a cyanobacterial bloom predicting method based on a non-linear kinetic time-series model, which belongs to the water environment predicting field. The method comprises the following steps: using the blue algae growth rate as a time-varying parameter; creating a non-linear kinetic time-series model for the cyanobacteria growth with double nutrient salt cycling; using the combination of the numerical algorithm and the intelligent evolutionary algorithm, optimizing the constant parameters in the non-linear kinetic time-series model for the cyanobacteria growth; through setting the multivariate time-series model to realize the prediction of the time-varying parameter and the cyanobacteria biomass and through using the bifurcation theory and the central manifold theory to make a nonlinear kinetic analysis of the cyanobacteria growth time-varying system, obtaining the outbreak conditions for a cyanobacteria bloom so as to make an early warning of the bloom outbreak. The method proposed by the invention not only determines the conditions for a cyanobacteria bloom outbreak, but also improves the bloom prediction accuracy, providing an effective reference for an environmental protection department and governance decisions for water environment treatment.
Owner:BEIJING TECHNOLOGY AND BUSINESS UNIVERSITY

Simulation system for spot welding invalidity number value

The invention relates to a spot-welding connection failure value simulation system in the car bodywork manufacturing engineering field. In the invention, a circle-stress failure criterion generating module obtains nugget circle stress distribution form according to the failure mode of the spot-welding connection in a strike process to generate the circle stress failure criterion; a failure extreme value stress and an index-parameter obtaining module obtain welding-spot critical failure stress extreme values and dimensionless stress sub-item index initial values under the condition of the peak values of four exterior loads; four types of sample value models which are pulling-cutting, pulling-extending, pulling-bending and pulling-twisting are established in a welding-spot connection value simulation module; an explicit dynamics analysis module couples circle stress failure criteria and obtains the continuous distributed inner stress of a welding-spot unit model and an extreme value stress borne by the welding-spot unit during failure time by simulation; a welding-spot failure material databank module stores the critical failure stress extreme values and the dimensionless stress sub-item index initial values of each stress component. The system not only can enhance the impact simulation precision without impact on the calculation efficiency, but also can reduce the design and exploitation cost.
Owner:SHANGHAI JIAO TONG UNIV

Method for converting data between ADAMS software and Pro/E software

The invention discloses a method for converting data between ADAMS software and Pro/E software, which comprises the following steps: firstly, performing kinematics and kinetics analysis by using an ADAMS, and when dimension parameters of a part model need to be changed according to the analysis result or design requirement, using ADAMS macro command and operating system batch processing command statements to directly start three-dimensional parameter modeling software Pro/E from the ADAMS; secondly, finishing automatic modification, reconstruction and virtual assembly of a three-dimensional complete machine or the part model in the Pro/E, applying constraint by using an interface module MECH/Pro, and finally adopting a command statement of Pro/TOOLKIT to automatically return to the ADAMS from the Pro/E; thirdly, performing the kinematics and kinetics analysis again, outputting a result if the requirement is satisfied, otherwise, repeating the steps until the requirement is satisfied; and fourthly, in the ADAMS software, outputting and storing dimension data of a module to be modified in the form of an independent data file. The method provides an automatic, simple and convenient, highly-efficient and reliable solution for mechanical design and analysis, and improves the design precision and the design efficiency of products.
Owner:CHINA AGRI UNIV

Global-local hybrid unmanned ship path planning method based on dynamic constraints

The invention provides a global-local hybrid unmanned ship path planning method based on dynamic constraints. The global-local hybrid unmanned ship path planning method comprises the steps of: S1, constructing an unmanned ship kinematics model, and conducting kinetic analysis; S2, considering a safety range of an unmanned ship, realizing the planning of a global path of the unmanned ship by adopting a storage node mode, and constraining the safe driving of the unmanned ship by optimizing the generated path points; S3, for a dynamic unpredictable environment, constructing a hierarchical structure based on an FDM fuzzy decision module and an FDW precise dynamic window module, and realizing the planning of a local path of the unmanned ship, precisely taking drivable forward, heading angular velocities and acceleration into account in the planning of the local path, and generating a traceable path that enables real-time local collision avoidance; S4, and fusing a global path planning scheme and a local path planning scheme of the unmanned ship to form a global-local hybrid obstacle avoidance strategy. According to the global-local hybrid unmanned ship path planning method, virtual pathpoints are inserted into the global optimal path, so that global and local path planning is perfectly combined, and the whole path tracking task is completed.
Owner:DALIAN MARITIME UNIVERSITY

Method for calculating rotor dynamics performance of multi-parallel-axis system

The invention relates to a method for calculating rotor dynamics performance of a multi-parallel-axis system. The method comprises the steps specifically as follows: step (1), selecting an analysis object and a calculation type, inputting parameters of a bearing-rotor system, finishing pre-processing operations like discretization of the rotor system; step (2), calling a bearing calculation program, calculating dynamic and static characteristic parameters of each bearing, forming a rotor dynamics equation of a parallel axis system which gives consideration to gear engagement according to the selected analysis object and calculation type; and step (3), calling a solving function to calculate a feature value and a feature vector of a dynamics differential equation, converting the feature value and the feature vector into dynamics characteristic result data through dimension so as to finish calculation and analysis of system stability, critical rotation speed, forced vibration response and vibration mode. According to the method disclosed by the invention, calculation and analysis means for dynamics performance of the multi-parallel-axis system, which can be applied to actual engineering, are developed on the basis of solid theoretical research; the calculated rotor system comprises supports of various types; therefore, combination of bearing calculation and rotor system dynamics analysis is implemented better.
Owner:XI AN JIAOTONG UNIV
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