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45 results about "Singularity avoidance" patented technology

Teleoperated robot for flood-welding operations

A remote controlled, tele-operated welder includes a multi-axis robot arm, video cameras, sensors a specialized control station that allows an operator to perform flood-fill welding operations at a remote location to avoid the heat, smoke and other environmental effects produced through typical flood-welding operations. The operator accesses the control unit (OCU) using a GUI and mouse, keyboard, joystick, or other custom controls, and observe the piece via the cameras (visual, thermal, or other) placed in the welding station via a feed displayed on the OCU display(s). Audio, video, and / or tactile feedback may be provided to indicate arm, welder, or other system status, for collision warning and arm motion singularity avoidance. Augmented reality informational graphic / textual overlays may provide guidance to an operator, and the apparatus may further include the ability to repeat series of steps needed to handle flood-weld on a given piece, repeatedly across many pieces.
Owner:HAMMOCK DARRYL

A path programming method for a plane redundancy robot to avoid obstacles and avoid singularities

A path programming method for a plane redundancy robot to avoid obstacles and avoid singularities relates to the field of robot motion control, and especially relates to a plane redundancy robot to avoid obstacles and avoid singularities. The invention aims to solve problems that risk of hurting working personnel by existing plane redundancy robots exists in a cooperation process and the speed of joints will exceed a robot allowance scope when the end of the robot moves to a singular position. The method of the invention is carried out according to the following steps: the method of the invention relates to threads which are carried out simultaneously: the first thread relates to several steps of path programming to avoid obstacles; and the second thread relates to various steps of path programming to avoid singularities. The method of the invention ca simultaneously complete the path programming method of obstacle avoidance and singularity avoidance, so that in a cooperation process, collaborator avoidance can be completed, and avoiding of singular configuration of the robot can also be realized to reduce risks of man-machine cooperation and raise the assembling quality. The method of the invention can be applied to the field of robot motion control.
Owner:HARBIN INST OF TECH

Control moment gyro singularity avoidance method based on instruction moment vector adjustment

A control moment gyro singularity avoidance method based on instruction moment vector adjustment comprises the steps of first acquiring a frame angular vector of control moment gyros, then calculating a Jacobian matrix, a singularity metric value and an instruction moment vector adjustment coefficient of a control moment gyro motion equation, next obtaining a control moment instruction adjustment vector and a zero motion singularity avoidance strength coefficient based on a control moment instruction given by an attitude controller, and finally obtaining a control moment gyro frame angular velocity instruction vector based on the control moment instruction adjustment vector and the zero motion singularity avoidance strength coefficient so as to control the moment gyro frame angular velocity. The invention overcomes the situation in which a moment instruction coincides with a particular direction thereof when a frame is "locked", thereby making separation impossible; solves the problem of a "locked" frame angle during singularity avoidance in the prior art; and achieves effective avoidance of the control moment gyro singularity.
Owner:BEIJING INST OF CONTROL ENG

Teleoperation system fractional order sliding mode synchronous control method based on event trigger mechanism

The invention provides a teleoperation system fractional order sliding mode synchronous control method based on an event trigger mechanism. The method comprises the steps: building a kinetic model of a teleoperation system through considering external disturbance and parameter uncertainty; selecting master and slave robots, interactively establishing a teleoperation system through a communication network, and determining system parameters of the kinetic model; designing a fractional order nonsingular fast terminal sliding mode surface equation by utilizing the position tracking error and the fractional order calculus; setting trigger event conditions of master and slave robot information interaction, and designing an adaptive fractional order nonsingular fast terminal sliding mode controller based on a sliding mode; and designing a Lyapunov function for stability analysis, and proving the boundness of a closed-loop state signal of the system. According to the teleoperation system fractional order sliding mode synchronous control method, the singular problem can be solved, the degree of freedom of the controller is expanded, the convergence speed is increased, the control precision is improved, the buffeting problem existing in the integer-order sliding mode surface is reduced, the applicability is higher, the occupation of network bandwidth and communication resources is reduced, and the resource utilization rate is increased.
Owner:YANSHAN UNIV

Design method of double parallel configuration VSDGCMGs singularity avoidance steering law

ActiveCN102749846ASmooth changeGuaranteed output torque accuracyAttitude controlAdaptive controlSingularity avoidanceSteering law
The invention discloses a design method of double parallel configuration VSDGCMGs singularity avoidance steering law, which comprises the steps of: firstly creating a dynamical model of double parallel configuration VSDGCMGs, and then, analyzing the singularity states of the double parallel configuration VSDGCMGs, finally, creating a framework control target function based on a singularity measure function, creating a flywheel control target function based on rotating speed balance, and designing the double parallel configuration VSDGCMGs singularity avoidance steering law comprehensively considering the singularity avoidance, energy consumption and rotating speed balance. The design method disclosed by the invention can effectively guarantee the output moment precision of the double parallel configuration VSDGCMGs and lay the foundation for agile maneuver attitude control of spacecrafts.
Owner:BEIHANG UNIV

Layering singularity avoidance method of remotely operating mechanical arm

A layering singularity avoidance method of a remotely operating mechanical arm belongs to the field of robot remote operation. The invention aims to solve the problem that in the existing mechanical arm movement process, a single method is adopted to avoid singularity, and the normal motion trail of the mechanical arm cannot be effectively ensured. The singularity avoidance layer of operation state of the mechanical arm is divided into a good region, a transition area and a sick area according to the local condition sequence of a mechanical arm singularity degree measurement index. When the mechanical arm operates in a good area, the movement of an operator of a main end is guided in a virtual force feedback mode; when the mechanical arm operates in the transition area, a traditional trackreconstruction method is adopted to reconstruct the tail end track of the mechanical arm; and when the mechanical arm operates in a sick area, the tail end track of the mechanical arm is reconstructed by adopting an improved track reconstruction method. The method is used for avoiding singularity of a mechanical arm.
Owner:HARBIN INST OF TECH

Method for confirming motion mode of corresponding free node at singular configuration part of hinge bar system mechanism

The invention discloses a method for confirming the motion mode of a corresponding free node at a singular configuration part of a hinge bar system mechanism. The method comprises the following steps of: carrying out second-order derivation on a coordination function which is dependent from a mechanism to describe the corresponding free node variable quantity, to judge whether the second-order derivative is equal to zero or not at the singular configuration place, if the second-order derivative is equal to zero, the corresponding free node at the singular configuration part can move like a limiting mechanism; and if the second-order derivative is not equal to zero, the corresponding free node can move like a first-order infinite small mechanism. According to the method, the motion mode of the corresponding free node at the singular configuration place of the hinge bar system mechanism can be confirmed, the motion mode of the mechanism at the singular configuration place can be basically confirmed, the method is high in operability, the basis is provided for the singularity avoidance and the structure design of the novel space structure, and the research of the mechanism singularity and the motion bifurcation has an important impelling action, so that the method is wide in application prospect.
Owner:ZHEJIANG UNIV

Singularity avoidance method and device in force-controlled traction process for robot

ActiveCN108608427AAvoid reachingReduced operating experienceProgramme-controlled manipulatorSimulationOperability
The invention provides a singularity avoidance method and device in a force-controlled traction process for a robot. The method comprises the following steps: calculating the operability indexes of the target robot in real time; determining whether the target robot approaches to a singularity configuration or not according to the operability indexes; and if the target robot is determined to approach to the singularity configuration, calculating a constraint force on the basis of the operability indexes, and additionally applying the constraint force onto the target robot through a driver, so that the target robot avoids the singularity configuration and continues to move under the effect of the constraint force. The method is capable of effectively preventing the robot from arriving at thesingularity configuration, and enabling the force-controlled traction process to be continuously carried out, so that the operation experience of force-controlled traction is improved, the operationefficiency of the force-controlled traction is increased, and the technical problems of low operation efficiency and poor operation experience of force-controlled traction due to the alarming and stopping of a robot, which are caused by that an operator drags the robot to a singularity configuration, are alleviated.
Owner:SIASUN CO LTD

Method for determining gimbal angular velocity of SGCMGs

ActiveCN110723316ASolve the problem of losing attitude maneuver abilityHarmonized Singularity AvoidanceCosmonautic vehiclesSpacecraft guiding apparatusSingularity avoidanceAttitude control
Disclosed is a method for determining the gimbal angular velocity of SGCMGs. The method includes the steps of firstly, determining a nominal gimbal angular vector of the configurations of the n SGCMGsaccording to the configurations and synthesis angular momentum of the n SGCMGs; secondly, determining the Jacob of a gimbal angular motion equation and the deviation of each gimbal angle deviating from nominal according to the gimbal angle of each SGCMG; and thirdly, determining a gimbal angular velocity instruction of the SGCMGs according to the Jacob determined in the step 2) and the deviation,determined in the step 2), of each gimbal angle deviating from nominal. By considering the distance of each gimbal angle deviating from nominal, the gimbal angular instruction amplitude and moment output deviation, the method has the abilities of singularity avoidance in attitude maneuvering and gimbal nominal position returning after maneuvering, the contradiction between the CMG gimbal singularity avoidance and the attitude control moment is resolved, and the high maneuvering performance at the arbitrary attitude can be ensured.
Owner:BEIJING INST OF CONTROL ENG

Method for confirming motion mode of corresponding free node at singular configuration part of hinge bar system mechanism

The invention discloses a method for confirming the motion mode of a corresponding free node at a singular configuration part of a hinge bar system mechanism. The method comprises the following steps of: carrying out second-order derivation on a coordination function which is dependent from a mechanism to describe the corresponding free node variable quantity, to judge whether the second-order derivative is equal to zero or not at the singular configuration place, if the second-order derivative is equal to zero, the corresponding free node at the singular configuration part can move like a limiting mechanism; and if the second-order derivative is not equal to zero, the corresponding free node can move like a first-order infinite small mechanism. According to the method, the motion mode of the corresponding free node at the singular configuration place of the hinge bar system mechanism can be confirmed, the motion mode of the mechanism at the singular configuration place can be basically confirmed, the method is high in operability, the basis is provided for the singularity avoidance and the structure design of the novel space structure, and the research of the mechanism singularity and the motion bifurcation has an important impelling action, so that the method is wide in application prospect.
Owner:ZHEJIANG UNIV

General avoidance method and system for singular point of mechanical arm

ActiveCN113601512AOmit transform solverGuaranteed inverseProgramme-controlled manipulatorSingularity avoidanceJoint angle
The invention discloses a general avoidance method and system for a singular point of a mechanical arm, and belongs to the technical field of avoidance of singular points of mechanical arms. The technical problem to be solved is to provide the improvement of the general avoidance method for the singular point of the mechanical arm. According to the technical scheme for solving the technical scheme, the method comprises the following steps that a kinematic model of the mechanical arm is established, a reference joint coordinate system is established, the spinor of each joint is calculated according to the spinor theory, and a Jacobian matrix is solved; a condition number is calculated by using a joint angle value of a tracing point and the Jacobian matrix; the condition number is used for judging whether the mechanical arm is close to the singular point or not, and after it is judged that the mechanical arm is about to approach the singular point, the mechanical arm uses a singularity avoidance algorithm to calculate a singularity avoidance tracing point till the condition number of the Jacobian matrix of the generated tracing point meets the state of being away from the singular point and the tracing point returns to an original Cartesian trajectory again; and after the singularity avoidance trajectory is planned, smoothing processing and trajectory interpolation are conducted on the planned singularity avoidance trajectory, and a final singularity avoidance trajectory is obtained; The invention is applied to the mechanical arm.
Owner:TAIYUAN UNIV OF TECH

Method for Avoiding Singular Points in Five-Axis Machining Tool Trajectory

The invention discloses a method for avoiding singular points of a five-axis machining tool feeding track, which aims at solving the technical problem of low machining accuracy in the existing method for avoiding the singular points of the five-axis machining tool feeding track. The method adopts the technical scheme with the following steps of using a quaternion to express a conversion relationship between the tool axis direction and the reference direction, and projecting the quaternion onto a P plane, wherein a singular cone in the P plane corresponds to a singular circle with center of circle at the origin point; using a B spline to interpolate a projecting point in a two-dimensional plane; establishing a constraint optimization problem again, wherein a target function is a sum of squares of increments of control top points, the constraint is the distance between the point of the B spline to the origin point in the P plane to be greater than the radius of the singular circle, and an initial value of the control top point is the control top point of the B spline obtained by interpolation; linearly expressing the constraint of the constraint optimization problem by the increment of the control top point of the B spline, and using a quadratic programming theory to solve an optimal solution of the optimizing problem. The method has the advantage that the common constraint optimization problem is converted into the quadratic programming problem, so that the processing accuracy is guaranteed.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Compliant force control method and system for collaborative robot

The invention discloses a compliance control method and system for a collaborative robot, and the method comprises the steps: building a stable force control strategy model of the tail end of the collaborative robot; establishing a rigidity optimization strategy model of the collaborative robot; establishing a singularity avoidance model of the collaborative robot; establishing a real-time control quantity solution model based on the stable force control strategy model, the rigidity optimization strategy model and the singularity avoidance model, and performing real-time control quantity solution to obtain the real-time control quantity of the collaborative robot; and controlling the compliance of the collaborative robot based on the real-time control quantity. In the embodiment of the invention, high-precision control on the contact force can be realized, and the rigidity of the collaborative robot system can be improved in real time, so that flutter is inhibited; the system can be effectively prevented from falling into a singular position type, and meanwhile the joint angle and angular velocity limitation of the robot is met.
Owner:INST OF INTELLIGENT MFG GUANGDONG ACAD OF SCI

Steering law singularity avoidant spacecraft attitude control system

A spacecraft attitude control system for maneuvering law singularity avoidance, comprising an attitude task management unit, an attitude controller, an attitude measuring unit, a gyro group maneuvering law unit, a frame angle position measuring unit, a control moment gyro group and a spacecraft. The gyro group maneuvering law unit calculates the frame angular rate of the control moment gyro group through the control moment gyro angular momentum table, zero motion algorithm and pseudo-inverse maneuvering law algorithm, and uses the angular rate value as the given signal of the control moment gyro group, In order to improve the control accuracy of spacecraft attitude. The present invention introduces a steering law design method based on the look-up table method to select the frame angular rate and the initial value of the frame angular position, realizes the precise torque output of the control moment gyroscope group, and avoids the pseudo-inverse maneuvering law calculation method to obtain the control moment gyroscope frame angular rate The singularity problem generated in the process avoids the "deadlock" problem that occurs when the zero-motion algorithm and the robust pseudo-inverse steering law are iteratively calculated.
Owner:AEROSPACE DONGFANGHONG SATELLITE
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