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50results about How to "Improve trajectory tracking accuracy" patented technology

Trajectory tracking control method used for driverless vehicle

InactiveCN108622104AImprove rolling stabilityEliminate the effect of lateral deviation accelerationSteering partsExternal condition input parametersSteering wheelCornering force
The invention discloses a trajectory tracking control method used for a driverless vehicle. The method includes the following steps that the current position point of a vehicle body is confirmed according to a reference trajectory; a matching point nearest to the current position point of the vehicle is found, and the road curvature of the nearest matching point is obtained according to a two-point curvature obtaining method; according to the current position point of the vehicle and the nearest matching point, a trajectory tracking error is obtained through calculation and comprises a transverse error and a head pointing error; a dynamic model feeding back cornering force on the basis of front wheels is established, and the optimal feedback control rate is obtained by the adoption of an LQR control algorithm; and the cornering force of the front wheels is determined, a front wheel slip angle is obtained on the basis of a reverse tire model, and then the steering wheel angle controlledquantity is obtained and issued to a steering-by-wire system to achieve trajectory tracking control. By the adoption of the method, the stability of trajectory tracking control of the driverless vehicle is improved, the trajectory tracking accuracy is improved, the tire slip angle is restrained, and the possibility that the tire force of the vehicle is saturated under an extreme working conditionand therefore the vehicle loses stability is avoided.
Owner:HUBEI UNIV OF AUTOMOTIVE TECH

Robust neural network control system for micro-electro-mechanical system (MEMS) gyroscope based on sliding mode compensation and control method of control system

The invention discloses a robust neural network control system for a micro-electro-mechanical system (MEMS) gyroscope based on sliding mode compensation and a control method of the control system. The control system comprises a given trajectory generation module, a sliding mode surface definition module, a neural network controller, a weight adaptive mechanism module, a sliding mode compensator, an MEMS gyroscope system, a proportional-differential control module, a first adder and a second adder. The control method of the control system comprises the following steps of: establishing an MEMS gyroscope kinetic model based on a sliding mode surface, designing a controller structure, and designing an updating algorithm of a radial basis function (RBF) network weight, so that the trajectory of the MEMS gyroscope is tacked. By the control method, the influence of the unknown dynamic characteristic of the MEMS gyroscope and noise interference can be compensated on line, the vibration trajectory of the MEMS gyroscope completely follows a reference trajectory, and the anti-interference robustness and reliability of the system are improved; the updating algorithm of the network weight is designed on the basis of a Lyapunov stability theory, so that the stability of a closed-loop system is ensured; and a powerful basis is provided for expanding the application range of the MEMS gyroscope.
Owner:HOHAI UNIV CHANGZHOU

Manipulator actuator fault tolerant control system based on double-layer structure and method thereof

The invention uses the idea of hierarchical structure control optimization to provide a manipulator actuator fault tolerant control system based on a double-layer structure and a method thereof, which belongs to the technical field of automatic control. In order to reduce the computational complexity and improve the instantaneity, a discrete system model under an actuator fault is established in an expansion manner through Taylor series. An FDD unit is designed to initiatively deal with a fault problem. The estimated fault information is introduced into a fault model to realize active fault tolerance. Uncertainties of the actual system are considered. A feedback correction mechanism is used for compensation. A manipulator fault tolerant controller is composed of a trajectory planning layer and a tracking control layer. According to different control objectives of each layer, a controller is designed separately, which is more specific to the problem. The fault tolerant control of the double-layer structure can deal with the existing system constraints, has strong robustness, can effectively solve the problem of the constant deviation fault of a complex manipulator actuator, and ensures the stability and the control performance of the whole system.
Owner:NANJING UNIV OF POSTS & TELECOMM

Four-rotor aircraft flight control method based on backstepping method

The invention discloses a four-rotor aircraft flight control method based on a backstepping method. The four-rotor aircraft flight control method based on a backstepping method includes the steps: according to the principle of flight mechanics and aerodynamics, establishing a kinetic model of a four-rotor aircraft and simplifying the model: setting the aircraft as a rigid body, setting the structure of the aircraft to be completely symmetrical, setting the center of gravity of the aircraft to coincide with the center of the aircraft, taking the ground coordinate system as the inertia coordinate system, and ignoring changes in the curvature of the Earth and the acceleration of gravity; according to the kinetic model of the four-rotor aircraft, analyzing the coupling relation of the flight control system, and constructing a system control structure graph; and finally according to the kinetic model of the four-rotor aircraft and the system control structure graph, using the backstepping method, combining with the Lyapunov stability principle, and determining the feedback compensation control quantity of the system. The four-rotor aircraft flight control method based on a backsteppingmethod can stably control the position and the attitude of the four-rotor aircraft, and has the advantages of high trajectory tracking accuracy, high response speed, and high anti-interference capability.
Owner:NANJING UNIV OF SCI & TECH

Cantilever beam vibration control method based on back-stepping fuzzy sliding mode control

The invention discloses a cantilever beam vibration control method based on back-stepping fuzzy sliding mode control. The method comprises the following steps of building a dynamic cantilever beam mathematical model, and performing cantilever beam mathematical model conversion; designing a back-stepping sliding mode controller on the basis of a Lyapunov stability theory, and obtaining a sliding mode control law; designing a fuzzy self-adaptation system on the basis of the Lyapunov stability theory, and obtaining a fuzzy self-adaptation law; simultaneously inputting the output of the back-stepping sliding mode controller and the output of the fuzzy self-adaptation system into the cantilever beam mathematical model; feeding back the output of the cantilever beam mathematical model to the fuzzy self-adaptation system in real time, and ensuring the global stability. The method has the beneficial effects that the relying of a control system on the cantilever beam mathematical model can be avoided; the manufacturing errors and the environment interference are compensated; the parameter study and regulation can be controlled in time, and the global progressive stability of the whole control system is ensured, so that the system reliability and the parameter change robustness can be improved.
Owner:HOHAI UNIV CHANGZHOU

Precise trace tracking optimal control method for uncertain rehabilitation walking training robot

The invention discloses a precise trace tracking optimal control method for an uncertain rehabilitation walking training robot. According to the method, a kinetic model of an uncertain rehabilitation walking training robot system is built, a one-order low-pass filter is built, the integral estimation is carried out on the uncertainty influencing the trace tracking precision of the rehabilitation walking training robot, a controller is designed on the basis of a precise feedback linearization method, and a linearization model of the system is built; on the basis of trace tracking errors, speed tracking errors and energy quadrics, a quadratic performance index of the rehabilitation walking training robot system is designed, the optimal control method is adopted, the precise trace tracking of the rehabilitation walking training robot is realized, and the performance index is optimized. Output high-precision PWM (pulse width modulation) signals are provided for a motor driving unit, so that the robot realizes precise tracking on reference trace signals. The control method has the advantages that the uncertainty bound of the system does not need to be known, the trace tracking precision of the rehabilitation walking training robot can be improved, and in addition, the system performance reaches the optimum.
Owner:SHENYANG POLYTECHNIC UNIV

Industrial robot trajectory tracking system and method adopting neural network iterative compensation

ActiveCN112518753AImprove the accuracy of the inverse solutionImprove motion trajectory accuracyProgramme-controlled manipulatorWelding/cutting auxillary devicesControl engineeringSimulation
The invention discloses an industrial robot trajectory tracking system and method adopting neural network iterative compensation. The trajectory tracking system is connected with an industrial robot and a measurement device separately, and a follow-up target ball matched with the measurement device is installed on a flange at the tail end of the industrial robot. A trajectory planning module is connected with the input end of the industrial robot through an inverse solution compensation module, a neural network PID module and a robot input interface in sequence, and the output end of the industrial robot is connected with a PID control module through a robot output interface. The trajectory planning module is connected with an error analysis module, the error analysis module is connected with the output end of the measurement device through a measurement output interface, and a measurement control module is connected with the input end of the measurement device through a measurement input interface. By means of the industrial robot trajectory tracking system and method, the inverse solution precision of the robot is improved, the influence of joint errors on the motion trajectory precision is reduced, and the robot is controlled to move according to an expected trajectory through the robot input interface; and the industrial robot trajectory tracking system and method are suitable for occasions with high motion trajectory precision requirements, such as welding, spraying and polishing.
Owner:ZHEJIANG SCI-TECH UNIV

Passive intelligent tracking and positioning method and system, storage medium and tracking and positioning terminal

ActiveCN111601253AHigh precisionOvercoming the problem of low accuracy of human body tracking and positioningChannel estimationLocation information based serviceHuman bodyTerminal equipment
The invention belongs to the technical field of wireless communication and artificial intelligence, and discloses a passive intelligent tracking and positioning method and system, a storage medium, atracking and positioning terminal and Wi-Fi equipment for collecting CSI information. The method comprises: extracting a dynamic propagation path component of each multipath signal by an inter-antennaCSI conjugate multiplication algorithm; estimating the signal parameters of the dynamic propagation path of each multipath signal by a channel parameter estimation algorithm; in combination with an artificial intelligence algorithm, each Wi-Fi device independently estimating a human body motion trail; and fusing the human body motion trails obtained by different Wi-Fi devices in the step 4 by using a multi-device motion trail fusion algorithm. According to the method, multi-channel parameter combination is used for tracking the human body motion trail, and an artificial intelligence algorithmis combined, so that the problems of low precision and poor robustness in the prior art are avoided. According to the invention, a plurality of Wi-Fi devices are combined to carry out human body motion trail tracking, the problem of low human body tracking and positioning precision in the prior art is avoided, and the indoor human body passive tracking and positioning precision is improved.
Owner:XIDIAN UNIV

Path following model prediction control method, system and device, and storage medium

InactiveCN111824146AEnsure driving stabilityImprove autonomous driving safetyDriving safetyState-space representation
The invention discloses a path following model prediction control method, system and device, and a storage medium. The method comprises the following steps: constructing a state space model of a vehicle; determining a tire slip angle dynamic constraint, and obtaining tire slip angle information according to the tire slip angle dynamic constraint and the state space model; constructing a path following model of the vehicle, and obtaining front wheel rotation angle information of the vehicle according to the path following model, the state space model and the tire slip angle information; and carrying out path following control on the vehicle according to the front wheel rotation angle information. According to the embodiment of the invention, the tire slip angle can be restrained within a reasonable range under different road adhesion coefficients; and a vehicle trajectory tracking capability is brought into full play, trajectory tracking precision is improved while vehicle driving stability is ensured so that the vehicle automatic driving safety and the vehicle path following control accuracy are improved, the overall performance of the vehicle is increased, and the method, the system, the device and the storage medium can be widely applied to the technical field of vehicle cruise control.
Owner:WUHAN UNIV OF TECH

Combined sliding mode motion control method of flexible mechanical arm

The invention discloses a combined sliding mode motion control method of a flexible mechanical arm. Under multiple time scales, the motion control problem of the flexible mechanical arm with disturbance and system uncertainty is researched. Because the flexible mechanical arm has a multi-time-scale characteristic, a controller designed by applying a traditional method is easy to cause an ill-conditioned numerical value problem, and based on a singular perturbation theory, the flexible mechanical arm is modeled into a singular perturbation system with singular perturbation parameters and decomposed into a fast subsystem and a slow subsystem which describe rigid body motion and flexible vibration. Under the slow time scale, with consideration of the influence of external disturbance and parameter uncertainty on the system, a self-adaptive sliding mode controller (slow controller) with a disturbance observer is designed to track the trajectory of the flexible mechanical arm. Under a fasttime scale, a robust sliding mode controller is designed to achieve flexible vibration suppression in order to eliminate the influence of vibration states and the like under an unmodeled dynamic scaleand a slow time scale on the design of the controller. Finally, the slow controller and the fast controller are combined by using a singular perturbation theory to realize a dual control target of trajectory tracking and vibration suppression. The test results show that the method is high in robustness and good in control effect.
Owner:716TH RES INST OF CHINA SHIPBUILDING INDAL CORP

Unmanned ship group formation cooperative control method considering time-varying drift angle and attitude adjustment

The invention discloses an unmanned ship group formation cooperative control method considering a time-varying drift angle and attitude adjustment. The method comprises the following steps of establishing a unified unmanned ship group formation graph theory representation method; establishing a three-degree-of-freedom kinetic model and a kinematics model which are universal for the unmanned ship; giving an objective function of formation control according to the planned path, the attitude parameter and the expected course; according to the established kinetic model and kinematic model, constructing an expansion observer for model uncertainty and external disturbance estimation; and according to the established expansion observer and the control target, designing an unmanned ship formation cooperative active-disturbance-rejection control law. The anti-disturbance control method based on linear tracking is provided, the self-adaptive control rate is given, time-varying drift angle compensation and attitude adjustment of the unmanned ship group formation are achieved, and therefore integrated regulation and control of formation position tracking and attitude adjustment of the unmanned ship group can be achieved.
Owner:GUANGDONG INTELLIGENT ROBOTICS INST

Cantilever beam vibration control method adaptive to H-infinite control

The invention discloses a cantilever beam vibration control method adaptive to H-infinite control, and is applied to cantilever beam vibration control. The method comprises the following steps: 1, establishing a model of a cantilever beam; 2, establishing a self-adaptive controller, and taking control output of the self-adaptive controller as control input of a cantilever beam system; and 3, based on a Lyapunov stability theory, establishing an adaptive law so as to ensure the system stability. The controller is composed of two parts, one part employs the self-adaptive controller to approach ideal control input of the cantilever beam system, and the other part employs an H-infinite robust controller to improve the robustness of the system for uncertainties and external interference. According to the invention, parameters of the controller can be adjusted in real time due to external interference uncertainties, and a given reference locus is accurately tracked, and tracking errors are rapidly convergent to be zero; and the controller designed based on a Riccati-like equation can effectively eliminate the influence exerted by system nonlinearity on locus tracking, can realize satisfying tracking performance of the cantilever beam system, and at the same time, improves the system robustness and reliability.
Owner:HOHAI UNIV CHANGZHOU

Fault-tolerant control system and method for manipulator arm actuator based on double-layer structure

The invention uses the idea of hierarchical structure control optimization to provide a manipulator actuator fault tolerant control system based on a double-layer structure and a method thereof, which belongs to the technical field of automatic control. In order to reduce the computational complexity and improve the instantaneity, a discrete system model under an actuator fault is established in an expansion manner through Taylor series. An FDD unit is designed to initiatively deal with a fault problem. The estimated fault information is introduced into a fault model to realize active fault tolerance. Uncertainties of the actual system are considered. A feedback correction mechanism is used for compensation. A manipulator fault tolerant controller is composed of a trajectory planning layer and a tracking control layer. According to different control objectives of each layer, a controller is designed separately, which is more specific to the problem. The fault tolerant control of the double-layer structure can deal with the existing system constraints, has strong robustness, can effectively solve the problem of the constant deviation fault of a complex manipulator actuator, and ensures the stability and the control performance of the whole system.
Owner:NANJING UNIV OF POSTS & TELECOMM

Spacecraft tracking control method based on integrated linear operator and anti-saturation technology

The invention relates to a spacecraft tracking control method, in particular to a spacecraft tracking control method based on an integrated linear operator and an anti-saturation technology. The objective of the invention is to solve the problem of low attitude orbit tracking maneuvering control performance of a spacecraft caused by the fact that the spacecraft is subject to unfavorable working conditions such as inertia parameter uncertainty and input saturation in a short-distance space task. The method comprises the following steps: measuring and obtaining attitude and orbit states of a target and a tracking spacecraft, determining a relative pose configuration between the target and the tracking spacecraft, and obtaining a pose tracking error of the tracking spacecraft; determining a speed tracking error under a tracking spacecraft body coordinate system; defining a filtering error of the target and the tracking spacecraft under the coordinates of the tracking spacecraft body; introducing a linear operator, and determining an inertial parameter updating matrix; obtaining real-time estimation of inertial parameters; obtaining an anti-saturation auxiliary system state vector; and obtaining a control input vector to execute a pose integrated tracking control strategy. The method is applied to the field of spacecraft tracking control.
Owner:HARBIN INST OF TECH
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