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43 results about "Kinetic coupling" patented technology

Power transmission line wind vibration control method based on simulated random gust field calculation

A power transmission line wind vibration control method based on power transmission line iron tower and lead or ground wire integrated system model calculation and multi-dimensional random gust field simulation includes the steps: firstly, generating a wind load time history sample by the aid of harmonic synthesis to simulate a wind field based on a multi-dimensional random vibration theory; secondly, establishing a dynamic model of an integrated system of a tower, lead or ground wire and wind vibration control device, analyzing the initial state of a lead or a ground wire and setting boundary conditions of the model; thirdly, converting wind load into wind pressure, loading a power transmission tower and line system and calculating time history of axial stress and displacement of an iron tower rod by the aid of simulation software; and fourthly, analyzing and judging wind vibration strength and wind vibration suppression effects and improving control effects by the aid of an optimization scheme. On the basis of rigid-flexible dynamic coupling among a power transmission line tower, the lead and the ground wire and fluid-solid coupling between a random gust wind field and a tower and lead or ground wire system structure, the determined wind vibration control method has better implementation effects.
Owner:ELECTRIC POWER RES INST OF GUANGDONG POWER GRID +1

A one-two-dimensional hydrodynamic coupling method based on spatial topology

InactiveCN109284531AAdapt to coupled computing needsGeneralized treatment of flood dischargeClimate change adaptationDesign optimisation/simulationRiver networkControl line
The invention provides a one-two-dimensional hydrodynamic coupling method based on a spatial topology. The method comprises the following steps: constructing a one-dimensional hydrodynamic model comprising a one-dimensional river network model for simulating the flow of a river network and a water-crossing structure, and a one-dimensional pipe network model for simulating the flow of a city pipe network; constructing a two-dimensional hydrodynamic model used for meshing the region within the compilation range and control line to be analyzed, interpolating the mesh according to the topography of the region, and assigning the mesh attributes; performing surface-to-surface two-dimensional model coupling for a river course and a surface according to the one-dimensional river network model andthe two-dimensional hydrodynamic model; according to the one-dimensional pipe network model and the two-dimensional hydrodynamic model, performing one-two-dimensional model coupling for the urban surface and underground. The invention provides a perfect coupling mode, which is adapted to different flood coupling calculation requirements. Flexible one-two-dimensional coupled generalization model can well solve the generalization of streams and streets flood discharge.
Owner:CHINA INST OF WATER RESOURCES & HYDROPOWER RES +1

Dynamic motion generation and control method for biped robot

ActiveCN112051741APreserve the free swing characteristicNo need to actively pushAdaptive controlVehiclesWhole bodySimulation
The invention discloses a biped robot dynamic motion generation and control method which comprises the following steps: in a single-foot supporting period, establishing a whole-body dynamics feedbacklinearization controller to control the lengths of supporting legs and the pitching posture of an upper body so as to keep the dynamic motion characteristics of a biped robot; decoupling the kinetic coupling of the swinging leg and the whole body based on a whole body kinetic model, controlling the position of future observation planning by establishing a swinging leg prediction control model, giving a series of target points at the tail end of the future leg through the adjustment of the foothold, planning the tail end track of the swinging leg according to the environmental information, andadjusting the foothold of the movable leg in real time; taking the whole body dynamic moment control quantity of the supporting legs and the control moment of the swinging legs as the motion control input of the biped robot; according to the method, the dynamics of the biped robot is introduced into real-time planning and online control, a high-dimensional nonlinear system is decoupled, and the swinging legs are independently controlled to achieve dynamic stable movement.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Method for flight dynamics optimization of small unmanned aerial vehicle based on bionic flexible wing

The invention discloses a method for optimizing flight dynamics of a small unmanned aerial vehicle based on a bionic flexible wing, and belongs to the field of overall design and flight dynamics of small fixed-wing unmanned aerial vehicles. According to the method, the bionic flexible wing is designed by imitating geometric and structural features of wings of large gliding birds; based on the bionic flexible wing, the modal analysis is performed on the wing to obtain first few modes of torsion which are very significant; an obtained first few mode equation set and a flight dynamics equation set are synthesized, and aerodynamic coupled terms generated by the elastic deformation are added; the influence of the aeroelastic effect of the bionic wing on the coupled of the flight dynamics is obtained, and critical parameters are refined, signs and sizes of critical parameters are adjusted by adjusting the wing structure design without changing the fuselage structure arrangement and overall pneumatic layout, the coupling form of the aeroelasticity of the wing and the flight dynamics is adjusted to achieve the goals of reducing the short-cycle frequency, increasing the short-cycle dampingratio and slow downing the gust disturbance of the small unmanned aerial vehicle.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

A surface two-dimensional underground pipe network hydrodynamic coupling method based on spatial topology

The invention provides a surface two-dimensional underground pipe network hydrodynamic coupling method based on spatial topology, which comprises the following steps: inputting surface water data andunderground drainage system water flow data, and establishing surface-underground connection relationship according to the surface water data and underground drainage system water flow data; generating and optimizing grid elements; calculating surface runoff and drainage pipe network flow respectively; calculating the exchange water quantity of surface runoff and drainage pipe network flow; checking the calculated exchange water quantity to realize the hydrodynamic coupling of two-dimensional underground pipe network on the surface. The invention realizes the division of the unstructured meshof the analyzed area, has a plurality of unstructured mesh division functions, and can realize the discrete arbitrary complex geometric boundary of the unstructured mesh, the cross processing of the boundary, and the optimization of the mesh unit. Furthermore, the exchange quantity of surface runoff and drainage pipe network flow is calculated, and the coupling of surface flood model and underground pipe network model is realized.
Owner:CHINA INST OF WATER RESOURCES & HYDROPOWER RES +1

Supporting system for vibration test of on-board add-on pieces and design method thereof

ActiveCN107239630AEffectively assess dynamic strengthEnsure boarding safetyGeometric CADDesign optimisation/simulationJet aeroplaneSupporting system
The invention provides a supporting system for a vibration test of on-board add-on pieces and a design method thereof. The supporting system includes a structural supporting piece composed of a big girder and a counter weight, a hanger switching device and a free suspension device, wherein the hanger switching device is connected to the big girder of the structural supporting piece and a hanger for supporting an add-on piece separately, and used for indirectly installing the add-on piece on the structural supporting piece; the free suspension device is connected to the structural supporting piece, and used for suspending a combination of the structural supporting piece, the hanger switching device, the hanger and the add-on piece in a free simulation state. According to the supporting system for the vibration test of the on-board add-on pieces and the design method thereof, by utilizing the structural supporting piece, the dynamical coupling effect of add-on piece installation on an airplane is stimulated; by adopting actual boundary stimulation to conduct an on-hook vibration ground test of the add-on pieces, the dynamic strength of the add-on pieces can be effectively tested, and the boarding safety of the add-on pieces can be ensured.
Owner:BEIJING INST OF STRUCTURE & ENVIRONMENT ENG +1

Parallel-type satellite antenna attitude adjusting apparatus

PendingCN108110424ASimple kinematic solutionMotion control design is easyAntennasHigh level techniquesKinematic couplingElevation angle
The invention relates to a parallel-type satellite antenna attitude adjusting apparatus, and adopts two rotary parallel mechanisms which are not coupled. The parallel-type satellite antenna attitude adjusting apparatus comprises a fixed platform, a movable platform and three branch movement chains connecting the fixed platform and the movable platform. The first branch movement chain comprises four movement pairs, a first rotary pair, a second universal joint, a third movable pair and a fourth universal joint are successively distributed in a direction from the fixed platform to the movable platform. The second branch movement chain comprises three movement pairs, and a first arc movement pair, a second movement pair and a third universal joint are successively distributed in a direction from the fixed platform to the movable platform. The third branch movement chain comprises two rotary pairs with axes being perpendicularly intersected. The antenna is installed on the movable platformby virtue of a bolt, two servo motors separately independently control an elevation angle and an azimuth angle of the antenna, so that an attitude of the antenna can be adjusted. The parallel-type satellite antenna attitude adjusting apparatus solves the problems in the prior art that the kinetics solution is complicated due to the high kinetic coupling performance of the parallel connection mechanism for adjusting the satellite antenna attitude, the control and design are difficult and the like.
Owner:HENAN UNIV OF SCI & TECH

Constant-value disturbance torque compensation method and system for oblique-flying and large-inertia coupling satellite

The invention discloses a constant-value disturbance torque compensation method for oblique-flying and large-inertia coupling satellite. The compensation method comprises steps as follows: a satellite attitude dynamical equation is simplified in a steady state; X-axis gyroscopic torque and Z-axis gyroscopic torque are obtained according to a dynamical coupling relation of an X axis and a Z axis; offset angular momentum of the X axis and offset angular momentum of the Z axis are obtained according to the relation between the X-axis and Z-axis gyroscopic torque and constant-value disturbance torque; magnetic torquer unloading is performed according to the obtained offset angular momentum, and angular momentum offset is realized. With the adoption of the method for producing gyroscopic torque compensation through angular momentum offset, angular momentum offset is realized easily through magnetic dumping, management of the angular momentum of the system is controlled by compensating the constant-value disturbance torque, saturation of the angular momentum of the satellite can be avoided under the condition that the magnetic torquer is fixed, the problem of high probability of saturation of the angular momentum due to the constant-value disturbance torque in an angular momentum exchange attitude control system is solved, and the beneficial effect that the angular momentum offset is applied to magnetic dumping of satellite attitude control is realized.
Owner:SHANGHAI AEROSPACE CONTROL TECH INST

Construction method of ballast track-bridge dynamic coupling model

The invention discloses a construction method of a ballast track-bridge dynamic coupling model. The method comprises the steps that a ballast track bed discrete element model reflecting the complex shape and the contact relation of a railway ballast is established through a discrete element method, and the model is used for representing a particle unit accumulation structure, the contact force between particles and coupling surfaces and an equivalent node transplantation load; a continuous medium sleeper finite element model and a bridge finite element model are established by utilizing a multi-body finite element method, wherein the models are used for representing a continuum grid structure, node displacement deformation, surface node position coordinates and an element connection relationship; and a ballast track-bridge dynamic coupling model is constructed based on a discrete element and multi-body finite element coupling method. According to the method, the irregular shape and themutual meshing and stacking relation of the ballasts on the mesoscopic level are fully considered, meanwhile, the interaction between the macroscopic ballast bed and the upper and lower structures can be reflected, and refined simulation of the complex mechanical behaviors of the ballast track on the bridge under the train load effect is achieved.
Owner:BEIJING JIAOTONG UNIV

Method for building an integrated dynamic model of vehicle-ground coupling

InactiveCN103366048BTo achieve integrated couplingSolving Dynamic Coupling ProblemsSpecial data processing applicationsVehicle dynamicsElement model
The invention relates to a method for building an integrated vehicle and ground coupled dynamical model. According to the method, a many-body dynamic model of a vehicle and a finite element model of the ground are integrated in one model which covers the mechanical relationship between the vehicle and the ground mathematically on the one hand and represents the coupling relationship between the vehicle and the ground during the solving process on the other hand; the coordinates and total strain of the ground can be calculated out based on the mechanical relationship and the coupling relationship; then the elastic force vector Qs and the like of the ground can be calculated according to the mechanical property, yield equation, flowing criterion and deformation state of the ground; finally, a new calculation is performed after the elastic force vector is substituted in a formula VI, and the loop iteration is carried out to complete the counting process of all the deformation, motion and stress state of the vehicle and ground in the time domain. According to the method, the integrated coupling with a ground mechanical model of a non-individual body is realized, the dynamical coupling of the vehicle and ground is solved really, and the method is suitable for solving the problem of huge deformation of the ground, such as moulding deformation.
Owner:SHANGHAI NORMAL UNIVERSITY

Method for building integrated vehicle and ground coupled dynamical model

InactiveCN103366048ATo achieve integrated couplingSolving Dynamic Coupling ProblemsSpecial data processing applicationsElement modelDynamic models
The invention relates to a method for building an integrated vehicle and ground coupled dynamical model. According to the method, a many-body dynamic model of a vehicle and a finite element model of the ground are integrated in one model which covers the mechanical relationship between the vehicle and the ground mathematically on the one hand and represents the coupling relationship between the vehicle and the ground during the solving process on the other hand; the coordinates and total strain of the ground can be calculated out based on the mechanical relationship and the coupling relationship; then the elastic force vector Qs and the like of the ground can be calculated according to the mechanical property, yield equation, flowing criterion and deformation state of the ground; finally, a new calculation is performed after the elastic force vector is substituted in a formula VI, and the loop iteration is carried out to complete the counting process of all the deformation, motion and stress state of the vehicle and ground in the time domain. According to the method, the integrated coupling with a ground mechanical model of a non-individual body is realized, the dynamical coupling of the vehicle and ground is solved really, and the method is suitable for solving the problem of huge deformation of the ground, such as moulding deformation.
Owner:SHANGHAI NORMAL UNIVERSITY

A support system for vibration test of airborne external pendant and its design method

ActiveCN107239630BEffectively assess dynamic strengthEnsure boarding safetyGeometric CADDesign optimisation/simulationSupporting systemDynamic strength
The invention provides a supporting system for a vibration test of on-board add-on pieces and a design method thereof. The supporting system includes a structural supporting piece composed of a big girder and a counter weight, a hanger switching device and a free suspension device, wherein the hanger switching device is connected to the big girder of the structural supporting piece and a hanger for supporting an add-on piece separately, and used for indirectly installing the add-on piece on the structural supporting piece; the free suspension device is connected to the structural supporting piece, and used for suspending a combination of the structural supporting piece, the hanger switching device, the hanger and the add-on piece in a free simulation state. According to the supporting system for the vibration test of the on-board add-on pieces and the design method thereof, by utilizing the structural supporting piece, the dynamical coupling effect of add-on piece installation on an airplane is stimulated; by adopting actual boundary stimulation to conduct an on-hook vibration ground test of the add-on pieces, the dynamic strength of the add-on pieces can be effectively tested, and the boarding safety of the add-on pieces can be ensured.
Owner:BEIJING INST OF STRUCTURE & ENVIRONMENT ENG +1

Finite element solution optimization method for structural thermal response induced by re-entry aerodynamic environment

The invention discloses a finite element solution optimization method for structural thermal response caused by re-entry aerodynamic environment, which includes: discretizing the coupled control equation based on heat conduction and material thermoelastic dynamics through the finite element method and providing a corresponding algorithm flow; wherein, In the algorithm process, for time-dependent partial differential equations, the finite element method discretizes the spatial region first, and obtains the grid division of the solution region, and then differentially discretizes the time item. According to the iterative coupling relaxation calculation principle, step by step Advance to capture the vibration of structural materials in space and the nonlinear behavior of thermal response deformation of large spacecraft after de-orbiting and re-entry into a strong aerodynamic thermal environment. The present invention provides an optimization method based on the finite element method for solving thermal-mechanical coupling response, which is beneficial for analyzing and researching the thermal-mechanical coupling response of material structures under strong aerodynamic / thermal environments, and is conducive to carrying out the performance prediction of aircraft and spacecraft structures with simulation.
Owner:中国空气动力研究与发展中心超高速空气动力研究所 +2

A Hydrodynamic Coupling Method for Surface Two-dimensional Underground Pipe Network Based on Spatial Topology

The invention provides a surface two-dimensional underground pipe network hydrodynamic coupling method based on spatial topology, which comprises the following steps: inputting surface water data andunderground drainage system water flow data, and establishing surface-underground connection relationship according to the surface water data and underground drainage system water flow data; generating and optimizing grid elements; calculating surface runoff and drainage pipe network flow respectively; calculating the exchange water quantity of surface runoff and drainage pipe network flow; checking the calculated exchange water quantity to realize the hydrodynamic coupling of two-dimensional underground pipe network on the surface. The invention realizes the division of the unstructured meshof the analyzed area, has a plurality of unstructured mesh division functions, and can realize the discrete arbitrary complex geometric boundary of the unstructured mesh, the cross processing of the boundary, and the optimization of the mesh unit. Furthermore, the exchange quantity of surface runoff and drainage pipe network flow is calculated, and the coupling of surface flood model and underground pipe network model is realized.
Owner:CHINA INST OF WATER RESOURCES & HYDROPOWER RES +1

Space six-degree-of-freedom rigid-flexible dynamics decoupling device

The invention provides a space six-degree-of-freedom rigid-flexible dynamics decoupling device. One end of a rotor of a first linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of a first rotating voice coil motor through a first flange plate; one end of a stator of the first linear voice coil motor in the linear freedom degree direction is fixedly connected with a rotor of a second rotating voice coil motor through a second flange plate; one end of a rotor of a second linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of the second rotating voice coil motor through a third flange plate; one end of a stator of the second linear voice coil motor in the linear freedom degree direction is fixedly connected with a rotor of a third rotating voice coil motor through a fourth flange plate; and one end of a rotor of a third linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of the third rotating voice coil motor through a fifth flange plate. The decoupling device provides six complete degrees of freedom, thereby completing the decoupling work of dynamics coupling between rigid and flexible parts on a spacecraft and improving the flexibility of the posture of the spacecraft and track control.
Owner:HARBIN INST OF TECH

Hydraulic driving articulated-type legged robot inter-joint decoupling control method

The invention discloses a hydraulic driving articulated-type legged robot inter-joint decoupling control method. Mechanical hydraulic combination coupling is used as a hydraulic driving articulated-type legged robot coupling behavior for researching, a coupling model between the joints of the leg of the robot is established. The coupling degrees of the various branches of the joints of the leg are calculated, and the characteristics of the coupling between the joints of the hydraulic driving articulated-type legged robot are researched. According to the coupling relation between the joints of the leg of the hydraulic driving articulated-type legged robot, the mechanism dynamics coupling force of the various motion branched chains of the robot is decomposed into the hydraulic servo driving systems of the various joints by Jacobian matrix transformation decomposition, and is used as perturbed force of a hydraulic system, and then decoupling control of electro-hydraulic servo system is carried out to eliminate the cross-linking coupling influences of the whole robot systems. The mechanical hydraulic combination coupling is used as a hydraulic driving articulated-type legged robot coupling behavior for the researching, and a decoupling control scheme is designed, and therefore the control precision of the robot is improved, the system has good control performance, and the improvement of the dynamic performance and the automation level of the hydraulic driving articulated-type legged robot is facilitated.
Owner:HARBIN UNIV OF SCI & TECH

Two-freedom-degree rotation parallel mechanism

The invention discloses a two-freedom-degree rotation parallel mechanism. The parallel mechanism comprises a movable platform, a fixed platform, two driving branch chains and a suitable constraint branch chain, the two driving branch chains have the same structural form, and each driving branch chain is composed of a parallelogram structure, rotation pairs and ball pairs. The suitable restraint branch chain is formed by connecting a first rotating pair and a second rotating pair in series, wherein the axes of the first rotating pair and the second rotating pair are perpendicular. The third ball pair of the first driving branch chain is connected with a restraining connecting rod of the suitable restraint branch chain, and the sixth ball pair in the second driving branch chain is connected with the movable platform. The speed jacobian matrix of the parallel mechanism is a diagonal matrix, and in other words, one output motion of the movable platform is only controlled by the input motion of one driving pair, and the defect that the kinematics and dynamics coupling performance of a common parallel mechanism is high is overcome; and meanwhile, by introducing the suitable constraint branch chain, the overall stability and the bearing capacity of the parallel mechanism can be enhanced, the precision of the parallel mechanism can be improved, and uncontrollable errors can be controlled.
Owner:HENAN UNIV OF SCI & TECH

A rigid-flexible dynamic decoupling device with six degrees of freedom in space

The invention provides a space six-degree-of-freedom rigid-flexible dynamics decoupling device. One end of a rotor of a first linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of a first rotating voice coil motor through a first flange plate; one end of a stator of the first linear voice coil motor in the linear freedom degree direction is fixedly connected with a rotor of a second rotating voice coil motor through a second flange plate; one end of a rotor of a second linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of the second rotating voice coil motor through a third flange plate; one end of a stator of the second linear voice coil motor in the linear freedom degree direction is fixedly connected with a rotor of a third rotating voice coil motor through a fourth flange plate; and one end of a rotor of a third linear voice coil motor in the linear freedom degree direction is fixedly connected with a stator of the third rotating voice coil motor through a fifth flange plate. The decoupling device provides six complete degrees of freedom, thereby completing the decoupling work of dynamics coupling between rigid and flexible parts on a spacecraft and improving the flexibility of the posture of the spacecraft and track control.
Owner:HARBIN INST OF TECH
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