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30 results about "Velocity equation" patented technology

Flight icing numerical value simulation method of helicopter rotor wing

The invention relates to a flight icing numerical value simulation method of a helicopter rotor wing. The flight icing numerical value simulation method is mainly characterized by comprising the following steps that: a vorticity compensation force algorithm is added into a momentum equation and an energy equation in a single fluid model used for vortex movement used for simulating air-super cold water drop two-phase flows under a rotating coordinate system in rotor wing trail traces, and a centrifugal force and geostrophic force algorithm is added into a super cold water drop sliding velocity equation; a water film movement and icing model of the centrifugal force and the geostrophic force is considered; and the algorithms and the models are used for carrying out the flight icing numerical value simulation flow process of the helicopter rotor wing, wherein the model of single fluid two-phase flowing used for simulating the simulating air-super cold water drop movement is realized by a partial differential equation group for describing the movement of air and air-super cold water drop binary mixtures in a rotor wing tail trace flow field, and a two-phase flow slipping speed model. The condition that the quality and energy changes are generated in water films and ice layers because of the rotary movement of the rotor wing is considered in the model of the water film movement and icing process on the rotor wing surface, and the icing shape of the rotor wing surface is obtained.
Owner:TIANJIN AEROCODE ENG APPL SOFTWAREDEV

Dynamic mesh numerical solution method based on modified fluid motion equation

The invention relates to a dynamic mesh numerical solution method based on a modified fluid motion equation, and belongs to the technical field of optimization methods. The method comprises the following steps: introducing an original non-linear convective term inside a concept deconstruction equation of convection speed into a speed equation on the basis of a classic cauchy equation of motion; deriving a linear modified fluid motion equation so as to establish a dynamic mesh numerical iteration solver special for the modified fluid motion equation under a finite volume discretization method. The linear characteristic of the dynamic mesh numerical iteration solver achieves obvious advantage on solving the problem of an internal flow field of a rotary machine, namely the speed item coefficient a of an equation to be solved does not participate in the cyclical iteration process of a PISO algorithm any longer, the equation can be solved by only utilizing a dynamic mesh equation based on the convection speed w, flux change caused by mesh motion can be directly obtained through the convection speed, and thus a numerical calculation process becomes an iteration solution process of a simple speed item U and a pressure item p. The dynamic mesh numerical solution method disclosed by the invention has the characteristics of high operation efficiency, short calculating time and low operation cost aiming at the design calculation of the internal flow field of the rotary machine.
Owner:CHINA UNIV OF MINING & TECH

Speed estimation and friction identification method of four-wheel turning/driving vehicle

The invention discloses a velocity estimation and friction identification method of a four-wheel turning/driving vehicle. The velocity estimation and friction identification method comprises the steps that firstly, a vehicle body coordinate system O-XY is established; secondly, a vehicle kinetic equation is established; thirdly, a wheel kinetic equation is established; fourthly, a wheel velocity equation is established; fifthly, a wheel slip rate equation is established; sixthly, the longitudinal force and lateral force of a wheel are obtained; seventhly, a friction model is parameterized; eighthly, a kinematical equation describing the relation of the vehicle velocity, the yaw velocity and the acceleration is established; ninthly, an observer is designed under the situation that detectable signals z comprise the longitudinal acceleration ax, the lateral acceleration ay, the yaw velocity r, the wheel angular velocity wj and the steering wheel rotation angle delta i; tenthly, persistent excitation conditions are defined. According to the velocity estimation and friction identification method, the nonlinearity self-adaptation observer for estimating the vehicle longitudinal velocity and the lateral velocity is established, the tire road surface friction parameters are established in real time according to the change of road surface conditions, and the velocity is estimated more accurately.
Owner:SHANDONG COMP SCI CENTNAT SUPERCOMP CENT IN JINAN

Projectile nutation angle extraction method based on radar Doppler data

The invention relates to a projectile nutation angle extraction method based on radar Doppler data. The method is characterized by comprising the following specific steps of arranging a radar tail chasing distributed station at the side rear part of an artillery or a rocket artillery, carrying out tracking measurement on a flying artillery shell or a rocket artillery shell, and estimating the radial velocity of a centroid; calculating micro motion speeds; extracting a precession period; resolving a velocity vector; calculating the nutation angle of a projectile. According to the method, the difficult problem in nutation angle measurement of the flying projectile under the conditions of long distance is solved effectively, and the motion of the rotating projectile in the air includes micro motions relative to the centroid, such as precession and nutation, besides centroid motion; radar signals are subjected to periodic modulation, namely micro-Doppler effect, by the micro motions. Internal data of the radial velocity obtained through radar measurement contain information on the micro motions, such as nutation, a nutation angle curve of the projectile can be obtained through processing the internal data, and the nutation angle of the projectile is obtained through an established micro-motion velocity equation.
Owner:冷雪冰

Circuit modeling and simulation method representing terahertz quantum cascading laser device multimode effect

InactiveCN104156545AMeet the needs of optoelectronic hybrid simulationGuaranteed Simulation AccuracySpecial data processing applicationsCircuit modelingOptical power
The invention relates to a circuit modeling and simulation method representing the terahertz quantum cascading laser device multimode effect. The method includes the steps of firstly, establishing a multimode velocity equation set representing carrier transportation characteristics inside a THzQCL active layer; secondly, establishing a physical equation model representing the multimode effect inside the THzQCL; thirdly, obtaining a corresponding equivalent circuit model through variable substitution and simplification; fourthly, establishing an equivalent circuit model representing the electrical characteristics of the input end of the THzQCL; fifthly, establishing an equivalent circuit model representing the luminous power characteristics of the output end of the THzQCL; sixthly, establishing a circuit macro model which comprises an electrical port and an optical power output port, and conducting photoelectric property simulation and output spectral property testing on the basis of the circuit macro model. By means of the circuit modeling and simulation method, the influences of the temperature on various photoelectric properties of the THzQCL can be tested, and imitation and simulation for the photoelectric property and the output multimode effect of the THzQCL can be supported and achieved.
Owner:WUHAN UNIV

Method for measuring enzymatic activity by integration method and initial rate method

The invention relates to an enzymatic activity test method using combining integration and initial velocity method, which is characterized in that the classical initial velocity is measured when the concentration of initial substrate is 70% higher than that of the preset substrate, and the classical initial velocity is still within linearity range; when the substrate consumption proportion in 80% record period is higher than the lower limit required in integration, the fitting reaction curve of integral velocity equation is used to determine the maximum reaction velocity using reaction time as independent variable, then the maximum reaction velocity is calculated as the initial velocity with preset substrate concentration is 93%; meanwhile, the slope of classical initial velocity and computation initial velocity to the enzyme amount reaction curve; when the substrate consumption proportion of the coupling enzyme reaction system in 80% record period is higher than the lower limit required in integration, the fitting enzyme reaction curve is used to determine the initial velocity using corresponding numerical integral velocity equation, otherwise the classical initial velocity is directly measured; total time for the optimization monitoring reaction guarantees the combination of the two methods.
Owner:CHONGQING MEDICAL UNIVERSITY

Vertical deviation measuring method based on static correction

The invention discloses a vertical deviation measuring method based on static correction. The vertical deviation measuring method comprises the steps that an attitude, position and velocity equation,and a measuring equation of a combined system vertical deviation observation model are established; a static correction vertical deviation observation model is established; whether a carrier is in uniform motion or not is determined, and if the carrier is in uniform motion, then a position difference and a measured value of course angle correction are used as the measuring equation to correct a vertical deviation equation; otherwise, a velocity, the position difference, and the measured value of course angle correction are used as observations to correct the vertical deviation equation; and inertia system output state variables are statically corrected based on the corrected static correction vertical deviation observation model. According to the vertical deviation measuring method based on static correction, velocity information and position information are used as the observations, in the meantime, zero angle correction observations are added to limit a course angle error, constant zero offset of an angular velocity sensor is updated to reduce the course angle drift, and the problems that southern attitude error compensation during the combined system vertical deviation measuringis not satisfied and the course angle error increases with time are solved.
Owner:SOUTHEAST UNIV

Earthquake forward modeling method applicable to non-uniform motion water bodies

ActiveCN104483702AObserve reflexesAffects accurate calculationsSeismic signal processingEquation of stateObservation system
The invention provides an earthquake forward modeling method applicable to non-uniform motion water bodies. The method comprises the steps that firstly, data, observation systems and hypocenter parameters related to seawater and strata are acquired; secondly, starting from the mass conservation equation, the Euler equation and the adiabatic state equation, through an asymptotic method and a suitable assumption based on the seawater practical conditions, a first-order stress-velocity equation suitable for the non-uniform motion water bodies is derived; thirdly, a reasonable boundary condition is given; finally, a control equation and the boundary condition are discretized through high-precision finite difference, and the propagation process of seismic waves in the seawater and seabed elastic media is simulated. According to the method, the influences of the density, sound velocity and flow velocity in the seawater on propagation of the seismic waves are comprehensively considered, the propagation condition of the seismic waves in a complex marine environment can be truly reflected, and the method has high application value in marine oil-gas exploration, especially deepwater oil-gas exploration in the complex marine environment.
Owner:INST OF GEOLOGY & GEOPHYSICS CHINESE ACAD OF SCI

Kinematics and dynamics solving method of underactuated mechanism with flexible kinematic pair

InactiveCN106446481ASolution implementationOvercome the defect that the numerical solution cannot be obtainedDesign optimisation/simulationSpecial data processing applicationsKinematics equationsDynamic models
The invention relates to a kinematics and dynamics solving iterative algorithm of an underactuated mechanism with a flexible kinematic pair. The algorithm includes the following steps: 1) establishing a coordinate system of the mechanism; 2) defining mechanism parameters, establishing a kinematic model and a dynamic model of the underactuated mechanism, and obtaining a kinematic position equation, a kinematic speed equation, a kinematic accelerated velocity equation and a dynamic equation of the mechanism; 3) giving initial condition of each component and a motion law of an original dynamic object, solving the kinematic equations and the dynamic equation of the mechanism at the time of t0, and obtaining the motion law of each component and the driving force of the original dynamic object at t0; 4) solving the kinematic equations and the dynamic equation of the mechanism at the time of tj, and obtaining the motion law of each component and the driving force of the original dynamic object at tj; 5) repeating the step 4 for n times so as to obtain the motion law of all components of the mechanism and the driving force of the original dynamic object in a whole motion cycle, drawing point by point by MATLAB, and obtaining motion raw curve of each component and a driving force change curve of the original dynamic object.
Owner:HEBEI UNIV OF TECH

Circuit modeling and simulation method for characterization of multimode effects in terahertz quantum cascade lasers

The invention relates to a circuit modeling and simulation method representing the terahertz quantum cascading laser device multimode effect. The method includes the steps of firstly, establishing a multimode velocity equation set representing carrier transportation characteristics inside a THzQCL active layer; secondly, establishing a physical equation model representing the multimode effect inside the THzQCL; thirdly, obtaining a corresponding equivalent circuit model through variable substitution and simplification; fourthly, establishing an equivalent circuit model representing the electrical characteristics of the input end of the THzQCL; fifthly, establishing an equivalent circuit model representing the luminous power characteristics of the output end of the THzQCL; sixthly, establishing a circuit macro model which comprises an electrical port and an optical power output port, and conducting photoelectric property simulation and output spectral property testing on the basis of the circuit macro model. By means of the circuit modeling and simulation method, the influences of the temperature on various photoelectric properties of the THzQCL can be tested, and imitation and simulation for the photoelectric property and the output multimode effect of the THzQCL can be supported and achieved.
Owner:WUHAN UNIV

Velocity Estimation and Friction Identification Method for Four-Wheel Steering/Driven Vehicles

The invention discloses a velocity estimation and friction identification method of a four-wheel turning / driving vehicle. The velocity estimation and friction identification method comprises the steps that firstly, a vehicle body coordinate system O-XY is established; secondly, a vehicle kinetic equation is established; thirdly, a wheel kinetic equation is established; fourthly, a wheel velocity equation is established; fifthly, a wheel slip rate equation is established; sixthly, the longitudinal force and lateral force of a wheel are obtained; seventhly, a friction model is parameterized; eighthly, a kinematical equation describing the relation of the vehicle velocity, the yaw velocity and the acceleration is established; ninthly, an observer is designed under the situation that detectable signals z comprise the longitudinal acceleration ax, the lateral acceleration ay, the yaw velocity r, the wheel angular velocity wj and the steering wheel rotation angle delta i; tenthly, persistent excitation conditions are defined. According to the velocity estimation and friction identification method, the nonlinearity self-adaptation observer for estimating the vehicle longitudinal velocity and the lateral velocity is established, the tire road surface friction parameters are established in real time according to the change of road surface conditions, and the velocity is estimated more accurately.
Owner:SHANDONG COMP SCI CENTNAT SUPERCOMP CENT IN JINAN

Flight icing numerical value simulation method of helicopter rotor wing

The invention relates to a flight icing numerical value simulation method of a helicopter rotor wing. The flight icing numerical value simulation method is mainly characterized by comprising the following steps that: a vorticity compensation force algorithm is added into a momentum equation and an energy equation in a single fluid model used for vortex movement used for simulating air-super cold water drop two-phase flows under a rotating coordinate system in rotor wing trail traces, and a centrifugal force and geostrophic force algorithm is added into a super cold water drop sliding velocity equation; a water film movement and icing model of the centrifugal force and the geostrophic force is considered; and the algorithms and the models are used for carrying out the flight icing numerical value simulation flow process of the helicopter rotor wing, wherein the model of single fluid two-phase flowing used for simulating the simulating air-super cold water drop movement is realized by a partial differential equation group for describing the movement of air and air-super cold water drop binary mixtures in a rotor wing tail trace flow field, and a two-phase flow slipping speed model. The condition that the quality and energy changes are generated in water films and ice layers because of the rotary movement of the rotor wing is considered in the model of the water film movement and icing process on the rotor wing surface, and the icing shape of the rotor wing surface is obtained.
Owner:TIANJIN AEROCODE ENG APPL SOFTWAREDEV

A Seismic Forward Modeling Method Applicable to Heterogeneously Moving Water Body

ActiveCN104483702BObserve reflexesAffects accurate calculationsSeismic signal processingObservation systemEquation of state
The invention provides an earthquake forward modeling method applicable to non-uniform motion water bodies. The method comprises the steps that firstly, data, observation systems and hypocenter parameters related to seawater and strata are acquired; secondly, starting from the mass conservation equation, the Euler equation and the adiabatic state equation, through an asymptotic method and a suitable assumption based on the seawater practical conditions, a first-order stress-velocity equation suitable for the non-uniform motion water bodies is derived; thirdly, a reasonable boundary condition is given; finally, a control equation and the boundary condition are discretized through high-precision finite difference, and the propagation process of seismic waves in the seawater and seabed elastic media is simulated. According to the method, the influences of the density, sound velocity and flow velocity in the seawater on propagation of the seismic waves are comprehensively considered, the propagation condition of the seismic waves in a complex marine environment can be truly reflected, and the method has high application value in marine oil-gas exploration, especially deepwater oil-gas exploration in the complex marine environment.
Owner:INST OF GEOLOGY & GEOPHYSICS CHINESE ACAD OF SCI

Kinematics and dynamics solution method of underactuated mechanism with flexible kinematic pairs

The invention relates to a kinematics and dynamics solving iterative algorithm of an underactuated mechanism with a flexible kinematic pair. The algorithm includes the following steps: 1) establishing a coordinate system of the mechanism; 2) defining mechanism parameters, establishing a kinematic model and a dynamic model of the underactuated mechanism, and obtaining a kinematic position equation, a kinematic speed equation, a kinematic accelerated velocity equation and a dynamic equation of the mechanism; 3) giving initial condition of each component and a motion law of an original dynamic object, solving the kinematic equations and the dynamic equation of the mechanism at the time of t0, and obtaining the motion law of each component and the driving force of the original dynamic object at t0; 4) solving the kinematic equations and the dynamic equation of the mechanism at the time of tj, and obtaining the motion law of each component and the driving force of the original dynamic object at tj; 5) repeating the step 4 for n times so as to obtain the motion law of all components of the mechanism and the driving force of the original dynamic object in a whole motion cycle, drawing point by point by MATLAB, and obtaining motion raw curve of each component and a driving force change curve of the original dynamic object.
Owner:HEBEI UNIV OF TECH

Extraction method of projectile nutation angle based on radar Doppler data

The invention relates to a projectile nutation angle extraction method based on radar Doppler data. The method is characterized by comprising the following specific steps of arranging a radar tail chasing distributed station at the side rear part of an artillery or a rocket artillery, carrying out tracking measurement on a flying artillery shell or a rocket artillery shell, and estimating the radial velocity of a centroid; calculating micro motion speeds; extracting a precession period; resolving a velocity vector; calculating the nutation angle of a projectile. According to the method, the difficult problem in nutation angle measurement of the flying projectile under the conditions of long distance is solved effectively, and the motion of the rotating projectile in the air includes micro motions relative to the centroid, such as precession and nutation, besides centroid motion; radar signals are subjected to periodic modulation, namely micro-Doppler effect, by the micro motions. Internal data of the radial velocity obtained through radar measurement contain information on the micro motions, such as nutation, a nutation angle curve of the projectile can be obtained through processing the internal data, and the nutation angle of the projectile is obtained through an established micro-motion velocity equation.
Owner:冷雪冰

Method and device for determining target speed of S-shaped speed planning

PendingCN113721555ASolve the problems caused by the complexity of solving the parameters of the objective functionImprove real-time performanceNumerical controlNumerical controlSimulation
The invention provides a method and device for determining the target speed of S-shaped speed planning, which belongs to the technical field of numerical control machining. The method comprises steps of acquiring cutter motion parameters, determining a target speed equation about the target speed according to the cutter motion parameters, solving the target speed equation by adopting a Lagrange interpolation method to obtain a target speed, and controlling the cutter to move according to the target speed. According to the method, a plurality of target function equations related to the target speed are obtained by analyzing the numerical relationship of each motion parameter under different values, and a method for solving the target function parameters by using the Lagrange interpolation method is provided for the target speed equation with the high-order term, the problem caused by complexity when a numerical value method represented by a bisection method and a Newton method is used for solving target function parameters is solved to a great extent, the real-time performance of the S-shaped speed planning process is improved, and the requirement for the hardware computing power of a numerical control machine tool is lowered.
Owner:SHENZHEN SHUMA ELECTRONICS TECH
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