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41 results about "Motion optimization" patented technology

Moving posture monitoring and guiding method and device based on multiple cameras

The invention relates to a moving posture monitoring and guiding method and device based on multiple cameras. The method comprises the following steps: acquiring moving images and/or video data of atleast one target sporter through a plurality of cameras; recognizing a target sporter from the moving image and/or the video data through a posture recognition algorithm, and outputting a human body posture graph required by moving posture monitoring; reconstructing human body three-dimensional posture information of the target sporter through a three-dimensional reconstruction algorithm based onthe human body posture diagram; carrying out skeleton registration on the target sporter and the reference person by utilizing the posture key nodes in the three-dimensional space; comparing the humanbody three-dimensional posture information of the target exerciser after bone registration with the human body three-dimensional posture information of the reference exerciser at a certain moment orwithin a preset time period; evaluating the action completion degree and quality of the target sporter based on the comparison result; and providing feedback to the target sporter based on the evaluation result, the feedback including whether the action reaches the standard and/or a motion optimization suggestion.
Owner:董秀园

Seven-degree-of-freedom mechanical arm limiting optimization method based on position-level inverse kinematics

ActiveCN112091979ASolving Inverse Solving ProblemsTake advantage of redundancyProgramme-controlled manipulatorOptimal controlIterative method
The invention provides a seven-degree-of-freedom mechanical arm limiting optimization method based on position-level inverse kinematics, and relates to a seven-degree-of-freedom mechanical arm limiting optimization method. The method aims to solve the problems that an existing numerical solution cannot obtain a closed solution, and final-state self-motion exists; and an analytical solution cannotbe used for offset configuration, and motion optimization cannot be realized. The method comprises the steps that firstly, an analytical solution of seven-degree-of-freedom mechanical arm inverse kinematics is obtained based on a parametric solving method for fixing a certain joint angle; then, the fixed joint angle parameter is used as input, joint limiting is used as an optimization index, and an optimal control problem is established; then, a constrained problem is converted into an unconstrained problem based on a Lagrangian multiplier method; and finally, the optimal joint angle parameteris solved based on a Newton iteration method, and seven joint space trajectories considering joint limiting optimization are obtained by giving an initial configuration, an expected tail end pose anda Cartesian path planning. The method is used for limiting optimization of a seven-degree-of-freedom mechanical arm.
Owner:HARBIN INST OF TECH

General method for machining complex curved surface of non-spherical cutter in multi-axis-linkage CNC manner

The invention discloses a general method for machining the complex curved surface of a non-spherical cutter in the multi-axis-linkage CNC manner. The method comprises the steps of (1) designing the curved-surface generating motion of a cutter relative to a workpiece: firstly, the curved surface of the cutter is described based on a vector function having continuous third-order partial derivatives, and then an envelope surface equation formula for the curved surface of the cutter is obtained with boundary conditions taken into consideration; secondly, a motion optimization functional extremum model formula of the cutter relative to the workpiece and having a minimum machining error, and a motion optimization functional extremum model formula of the cutter relative to the workpiece and having a maximum machining line width are obtained; finally, the above functional extremum model formulas are solved to respectively obtain a motion of the cutter relative to the workpiece at a given machining line width and a minimum curved-surface machining error, and a motion of the cutter relative to the workpiece at a maximum machining line width and a given limit error; (2) realizing the curved-surface generating motion of the cutter relative to the workpiece on a specific machine tool. According to the technical scheme of the invention, the machining accuracy and the machining efficiency of the curved surface are improved through fully developing the machining potential of the multi-axis-linkage CNC.
Owner:GUILIN FUDA GEAR +1

Motion optimization based self-instruction generating method for imaging satellite

ActiveCN106371448AReduce execution complexityImproved ease of handlingCosmonautic vehiclesCosmonautic partsGreedy algorithmOrbit
The invention discloses a motion optimization based self-instruction generating method for imaging satellite, a method of converting multiple meta-tasks into on-satellite manipulation-level instructions. According to the method, firstly, based on the motion information equipped to the meta-tasks and the timing sequence relationships among the meta-tasks and through the use of the greedy algorithm, the same type of motions of opening and closing the machine between two adjacent meta-tasks are maximized. Therefore, the execution complexity of software is reduced; the motion sequence of the satellites is effectively planned. And according to the motion sequence and the working state of the current satellite's equipment (for instance, sequestration uses backup to save, digital transmission servo uses the original, and etc.), the corresponding manipulation-level instructions are specified so as to effectively make the satellites more operational, achieve better efficiency and provide technical support to enable the single orbit of agile satellites to complete multiple tasks. In addition, according to the method, abstract definitions are made between the meta-tasks and their corresponding motion information as well as between the timing sequence relationships of the meta-tasks, which allows a user to define themselves. Therefore, the method is very flexible and universal and can be applied to various remote sensing satellites.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

Non-contact emotional recognition method based on dual-mode sensor

The invention discloses a non-contact emotional recognition method based on a dual-mode sensor, wherein the non-contact emotional recognition method comprises the following steps: obtaining vital signsignals from echo signals collected by radar sensors, and extracting breathing signals and heartbeat signals from the signals; selecting a human face region from video images collected by video sensors, and obtaining the heartbeat signals and optical flow vector signals according to the human face region; for the heartbeat signals, carrying out heartbeat optimization treatment based on a light intensity method; based on the optical flow vector signals, carrying out body motion optimization treatment on the breathing signals obtained by the radar sensors; for the optimized heartbeat and breathing signals, carrying out characteristic extraction; carrying out characteristic selection on heartbeat characteristics and breathing characteristics, and establishing an emotion recognition model according to the screened characteristics; and according to the emotion recognition model, recognizing the emotion to be recognized. The non-contact measurement not only cannot introduce discomfort, butalso can reduce measurement error, and has the advantages of high recognition accuracy, good robustness and wider applicability.
Owner:NANJING UNIV OF SCI & TECH

Optimization method for automatically forming cutting motion of section of cantilever longitudinal shaft type heading machine

The invention discloses an optimization method for automatically forming a cutting motion of the section of a cantilever longitudinal shaft type heading machine. The optimization method comprises the following steps of establishing five coordinate systems in a roadway, calculating the coordinate of the ith cutting tooth of a cutting head in an O0-X0Y0Z0 coordinate system according to the coordinate of the ith cutting tooth of the cutting head in an O3-X3Y3Z3 coordinate system, planning the track of the cutting head during horizontal movement by adopting a high-order polynomial transition linear interpolation method, planning the track of the cutting head during non-horizontal movement by adopting a combined sine function curve, and then determining a coordinate sequence of all inflection points on the section of the roadway in a cutting path according to the form of the section of the roadway. According to the optimization method, a correction method is provided for the inflection point positions of the S-shaped cutting paths of different roadway section types, the forming precision of the sections can be further increased, and the method is easy to implement through programs in an automatic section forming control system.
Owner:CHINA UNIV OF MINING & TECH

CMG group return nominal configuration control method and system based on zero motion optimization and medium

ActiveCN111891401AImprove balanceSolve the problem of snapping back to the nominal frame corner positionCosmonautic vehiclesSpacecraft guiding apparatusSpacecraft attitude controlAngular velocity
The invention discloses a CMG group return nominal configuration control method and system based on zero motion optimization, and a medium, which belong to the technical field of spacecraft attitude control. The method comprises the steps of firstly calculating a frame angular speed reference value according to the frame angular deviation through employing zero motion; and then setting a dynamic return nominal adjustment factor value according to the length of the frame angular deviation vector, so that the integrated frame angular speed is larger when the frame angular deviation is large, andthe integrated frame angular speed is smaller when the frame angular deviation is small. By adopting the method, the problem that the CMG group frame angle is quickly adjusted to the nominal positionunder the condition that the satellite does not influence normal control is well solved. Aiming at the multi-redundancy condition of the CMG group, the high efficiency and rapidity of CMG return nominal are realized in a zero motion mode by utilizing different zero space vector combinations, and the problem that the framework angle of an agile satellite control moment gyro rapidly returns to thenominal position, which is not solved in the prior art, is solved.
Owner:BEIJING INST OF CONTROL ENG

Joint locking failure space manipulator halt optimizing method

ActiveCN111923037AAchieving Comprehensive RepresentationProgramme-controlled manipulatorJointsControl theoryJoint locking
The invention provides a joint locking failure space manipulator halt optimizing method which comprises the following steps: according to all exercise capacity indicators after standardized processingof a joint locking failure space manipulator, and based on an improved analytic hierarchy process and an entropy method, solving the weight of all exercise capacity indicators to realize comprehensive characterization of exercise capacity of the manipulator, constructing a preferable model of a joint locking failure space manipulator halt configuration, further solving a preferable model of the halt configuration based on the Monte Carlo numerical method, obtaining the optimal halt configuration of the joint locking failure manipulator, then, carrying out motion planning on the manipulator based on a sextic polynomial by taking the halt movement characteristics into consideration, further taking the safety and stability of the manipulator into consideration during the halt process, constructing and solving a space manipulator halt movement optimization model, and finishing halt optimization of the joint locking failure space manipulator. According to the technical scheme, safe and stable halt of the joint locking failure space manipulator can be realized.
Owner:BEIJING UNIV OF POSTS & TELECOMM

Passenger flow confluence walking behavior simulation method for station facility combination part

The invention provides a passenger flow confluence walking behavior simulation method for a station facility combination part. The method comprises the steps that the layout structure, the geometric dimension and the passenger flow streamline characteristics of a station facility combination part are obtained, and the station facility combination part is divided into a channel straight-going area,a stair area, a confluence area and an exit straight-going area; a classic social force model is used to simulate the walking behaviors of the passenger flow in the passage straight-going area and the exit straight-going area; a three-dimensional social force is introduced to simulate the walking behavior of the passenger flow in the stair area; attraction is introduced, and a turning social force model is used for simulating walking behaviors of pedestrians in a confluence area. According to the method, walking parameters under different scenes are simulated and quantified, the walking stateand the facility area passing rate are constructed to serve as indexes of bottleneck recognition through the relation between time and the layout structure and the geometrical attribute of a channel,and improvement suggestions are provided for confluence area passenger flow motion optimization and facility combination part design.
Owner:BEIJING JIAOTONG UNIV

A Method of Autonomous Command Generation for Imaging Satellite Based on Motion Optimization

ActiveCN106371448BReduce execution complexityImproved ease of handlingCosmonautic vehiclesCosmonautic partsGreedy algorithmOrbit
The invention discloses a motion optimization based self-instruction generating method for imaging satellite, a method of converting multiple meta-tasks into on-satellite manipulation-level instructions. According to the method, firstly, based on the motion information equipped to the meta-tasks and the timing sequence relationships among the meta-tasks and through the use of the greedy algorithm, the same type of motions of opening and closing the machine between two adjacent meta-tasks are maximized. Therefore, the execution complexity of software is reduced; the motion sequence of the satellites is effectively planned. And according to the motion sequence and the working state of the current satellite's equipment (for instance, sequestration uses backup to save, digital transmission servo uses the original, and etc.), the corresponding manipulation-level instructions are specified so as to effectively make the satellites more operational, achieve better efficiency and provide technical support to enable the single orbit of agile satellites to complete multiple tasks. In addition, according to the method, abstract definitions are made between the meta-tasks and their corresponding motion information as well as between the timing sequence relationships of the meta-tasks, which allows a user to define themselves. Therefore, the method is very flexible and universal and can be applied to various remote sensing satellites.
Owner:BEIJING INST OF SPACECRAFT SYST ENG

Point cloud global motion optimization method and device

The invention discloses a point cloud global motion optimization method, and the method comprises the steps that a motion matrix initial value of each visual angle is reconstructed into a low-rank sparse matrix, and then the matrix recovery is carried out; under the condition that any two visual angles are known to move, a universal constraint condition is put forward to be added into an iterationprocess, the iteration frequency is effectively limited, the algorithm efficiency is improved, and the influence caused by random noise is reduced; a Cauchy weight item is added to measure the reliability of pairwise visual angle measurement, the influence of outliers is effectively reduced, and the robustness of the algorithm is improved; the method is suitable for solving an accurate global motion problem of a known multi-view point cloud relative motion initial value and real values of any two view changes. The method aims to solve the problems that a multi-view point cloud global optimization method in dimensional reconstruction excessively depends on registration initial values, robustness is not high and efficiency is low, random noise and abnormal values in initial motion are eliminated, point cloud global motion recovery precision is improved, and a more accurate reconstruction model is obtained.
Owner:SUN YAT SEN UNIV
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