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204 results about "Equivalent control" patented technology

Automatic control system and method for preventing side-slipping and side-turnover in curve road

InactiveCN103121447AGuaranteed automatic decelerationGuaranteed feasibilityVehicle dynamicsKinematic controller
The invention relates to the safe auxiliary driving and intelligent control filed and discloses an automatic control system and a method for preventing side-slipping and side-turnover in a curve road. A vehicle-mounted automatic control system is adopted to control an intelligent vehicle. At first, information about curve road curvature is obtained; secondly, the information about curve road curvature is converted into digital signals and input into a vehicle-mounted micro-processor, curve road critical safe driving speed is calculated by a safe driving speed calculation module and current driving speed is measured by a vehicle-mounted sensor; then the current driving speed and the critical safe driving speed are judged by a safe condition judging module; and finally a system automatic control module is used to control the intelligent vehicle to pass through the curve road smoothly. The automatic control system and the method for preventing side-slipping and side-turnover in the curve road overcome the shortcoming that trajectory tracking is achieved by only using a vehicle kinematics controller, a designed vehicle dynamics controller guarantees straightaway automatic deceleration and practicability and instantaneity of maintenance in the curve road, and calculation accuracy of safe driving speed is improved. By means of dynamics control principles including equivalent control and switching control, the system chattering phenomenon can be restrained effectively and influence of external disturbances can be overcome.
Owner:DALIAN UNIV OF TECH

Similarity detection method of computer software source code

ActiveCN105426711AIncrease variableAccurately reflect the percentageProgram/content distribution protectionCoding blockEquivalent control
The invention relates to a similarity detection method of a computer software source code, and belongs to the technical field of computer application. The method comprises the following steps: firstly, according to different programming languages, carrying out a word segmentation operation on the source code; then, selecting a specific labeling word to carry out partitioning processing on a word segmentation result, and carrying out relevant processing on a variable segmentation word according to variable attributes; thirdly, on the basis of a word segmentation result, carrying out a difference measurement operation on each block to obtain a difference matrix, and obtaining integral difference according to the difference result and the correlation of each block; and finally, according to a formula, finally obtaining a code similarity detection result. Compared with the prior art, the method can successfully identify means including word-for-word copying, comment statement blank area change, identifier renaming, data type change and the like in the similarity detection of the code, and can successfully detect means that a code block sequence is changed, a statement sequence is changed, redundant statements and variables are increased, an original control structure is replaced with an equivalent control structure and the like.
Owner:北京众码教育科技有限公司

Flexible spacecraft underactuated system based on switching control method and attitude control method thereof

InactiveCN104460679AOvercoming limitations that make it difficult to work properlyImprove reliabilityAttitude controlNonlinear modelSpacecraft attitude control
The invention discloses a flexible spacecraft underactuated system based on the switching control method and an attitude control method of the flexible spacecraft underactuated system based on the switching control method and belongs to the technical field of spacecraft attitude control. According to the flexible spacecraft underactuated system based on the switching control method and the attitude control method of the flexible spacecraft underactuated system based on the switching control method, a dynamical model of a flexible spacecraft with an execution mechanism completely ineffective is established, coupling, caused by elastic vibration of a flexible accessory, with a rigid body is taken as an uncertainty of the system, a dynamical model of a conversion system is a standard nonlinear model, all states are divided into three sliding model surfaces according to the layering sliding model idea, an equivalent control component is designed for the first layer of sliding model surface according to the Filippov equivalent theorem, a switching control law is designed by means of the second layer of sliding model surface and the third layer of sliding model surface, and a final control law is formed by combining equivalent control input and the switching control law. By the adoption of the flexible spacecraft underactuated system based on the switching control method and the attitude control method of the flexible spacecraft underactuated system based on the switching control method, the defect that in the prior art, a flexible spacecraft can not operate normally under the condition that an actuator becomes ineffective completely during operating of the flexible spacecraft is overcome, and operating reliability of a flexible spacecraft attitude control system is improved.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Control method for sliding mode converter control structure of active power filter containing parameter perturbation

The invention discloses a control method for a sliding mode converter control structure of an active power filter containing a parameter perturbation, which comprises the following steps: firstly, building a state space mathematical model under an abc coordinate system; converting the state space mathematical model to be under a dq coordinate system to obtain a uniform mathematical model by taking dq components of harmonic current and capacitor voltage on a direct-current side as state variables; constructing a sliding mode surface; decoupling the sliding mode surface for control; defining a control rate; carrying out inverse transformation on the control rate to obtain an effective control rate; constructing an integral sliding mode surface; and redefining a new control rate, so as to finally obtain a PWM (Pulse-Width Modulation) signal for driving a switch tube. The control method adopts the sliding mode converter structure, so that current tracking and the capacitor voltage on the direct-current side are uniformly controlled. The sliding mode converter control structure is simple in design and is easy to realized, has good robustness on the internal parameter perturbation and internal interference of a system and has good dynamic performance, and the current variation can be quickly tracked when a load is suddenly changed.
Owner:UONONE GRP JIANGSU ELECTRICAL CO LTD

Balanced control distribution method of airplane with multiple control surfaces

The invention provides a balanced control distribution method of an airplane with multiple control surfaces, which mainly comprises the following steps of: transferring a control distribution problem of the multiple control surfaces into an equivalent control problem of a virtual control surface and a real control surface, determining a basic method for carrying out normalization on the real control surface and carrying out balanced distribution on the control efficiency, classifying the real control surface, carrying out the normalization and sequencing according to absolute values of the normalized control efficiency, determining the leading control efficiency of the virtual control surface, grading the normalized control surfaces, calculating a distribution coefficient and the like. Inthe invention, by utilizing the balanced control distribution method, the control of the multiple control surfaces is equalized to the control of the special control efficiency and the virtual control surface which is limited by a deflection range, so that the design of the control efficiency is simplified, the problem that the angular rate of the control surface is transfinite, and the matrix calculation of the weighted balanced distribution is simple; the deflection range, the control efficiency, the control grade and the authority coefficient of the control surface are comprehensively considered, and the effective control surface is completely utilized, so that the saturation, which is caused by that some control surfaces bear overmuch control efficiency, is effectively avoided.
Owner:BEIHANG UNIV

Dynamic sliding mode voltage control method for DC-DC boost converter based on interval type-II adaptive fuzzy neural network

The invention discloses a dynamic sliding mode voltage control method for a DC-DC boost converter based on an interval type-II adaptive fuzzy neural network, and relates to the technical field of power electronic control. The invention aims to solve the problem sliding mode control on the DC-DC boost converter based on a fuzzy neural network lacks robustness to complex uncertainty and autonomous learning capability of the fuzzy neural network in the prior art. The method comprises the steps of obtaining operating parameters of the DC-DC boost converter, and establishing a dynamic model of theDC-DC boost converter; adopting a tracking error dynamic system containing a dynamic sliding mode control law to track the output voltage in the dynamic model; designing a sliding mode surface according to the tracking error dynamic system to obtain a dynamic equivalent control law, and constructing a dynamic sliding mode controller based on the interval type-II adaptive fuzzy neural network according to the dynamic equivalent control law; and controlling the dynamic sliding mode control law through the controller to enable the output voltage in the tracking error dynamic system to be equal tothe expected voltage. The control method is used for controlling output voltage.
Owner:HARBIN INST OF TECH +2

Fixed-frequency quasi-sliding mode controller applicable to single-inductance double-output buck converter

InactiveCN102684490AIncrease the working range of the loadReduce in quantityDc-dc conversionElectric variable regulationControl signalEngineering
The invention discloses a fixed-frequency quasi-sliding mode controller applicable to a single-inductance double-output buck converter. The fixed-frequency quasi-sliding mode controller comprises an equivalent follow current duty ratio detector, a fixed-frequency quasi-sliding mode equivalent control signal generator, a first comparator comp1 and a dynamic follow current generation circuit, wherein the equivalent follow current duty ratio detector is used for detecting an equivalent follow current duty ratio signal of inductance current; the fixed-frequency quasi-sliding mode equivalent control signal generator is used for outputting a fixed-frequency quasi-sliding mode equivalent control signal; the first comparator comp1 is used for outputting a control signal D1 and a control signal D2 of a synchronous sequential tube S1 and a synchronous sequential tube S2; and the dynamic follow current generation circuit is used for generating a control signal of a follow current tube S3 and selecting follow current at the next moment according to an inductance current follow current duty ratio signal at the current moment. Compared with the controller in the prior art, the fixed-frequency quasi-sliding mode controller has the advantages that the problems of over-high voltage cross-modulation and low transient response speed in the single-inductance double-output buck converter can be solved, and the load working range of the single-inductance double-output buck converter can be greatly expanded on the premise of keeping high efficiency of a system and quick response.
Owner:ZHEJIANG UNIV

Voltage and current double closed loop control method and device of adjustable invertor inertial effect

ActiveCN106559005AAdjust the inertia effectEquivalent synchronization effectAc-dc conversionSingle network parallel feeding arrangementsInertial effectLow-pass filter
The present invention discloses a voltage and current double closed loop control method and device of an adjustable invertor inertial effect. In the frame of the routine voltage and current double closed loop control, the inertial current component is added in an inverter current inner ring instruction to realize the equivalent control of the inverter inertia property and is indirectly generated through an inertial control system connected in parallel on the voltage outer ring. The inertial control system is formed by three parts connected in series, wherein the three parts include a low pass filter, a proportional controller and a differential arithmetical unit. The size of the inertial current component and the intensity level of the grid-connected inverter inertial effect can be flexibly controlled through the proportional controller in the inertial control system. The voltage and current double closed loop control method of the adjustable invertor inertial effect does not need to change the hardware portion of the current grid-connected inverter system, completely maintains the current basic control frame of the software portion, has good compatibility, can be applied to a double-fed wind turbine system and a photovoltaic power generation system, and has good engineering application values.
Owner:NANJING INST OF TECH

Discrete repetition sliding mode control method for inverter

According to a discrete repetition sliding mode control method for an inverter, a difference between preset inverter voltage and actual inverter voltage is used as a repetition sliding mode controller error; the preset inverter voltage is as an input of a feedforward transfer function and an index double-power approach rate; a summation of a repeated controlled output and a repeated sliding mode controller error is used as the input of the sliding mode controller on the condition of equivalent control; and a summation of the output of the feedfoward transfer function, the output of the sliding mode controller and the output of the index double-power approach rate is used as a control signal for switching on or switching off an inverter bridge switch tube in an inversion step. According to the discrete repetition sliding mode control mode, repeated control and sliding mode control are combined based on an equivalent control method in a discrete domain, thereby realizing advantages of high state precision in repeated control and high dynamic speed and high robustness in sliding mode control. Furthermore the index double-power approach rate can improve system dynamic response speed. According to the discrete repetition sliding mode control method, designing is performed in the discrete domain, and a result more accords with an actual system.
Owner:TAIYUAN UNIV OF TECH

Unified power flow controller equivalent modeling method based on switching period average principle

The invention relates to the technical field of electric system modeling and analysis, in particular to a unified power flow controller equivalent modeling method based on the switching period averageprinciple. The method comprises the steps that a unified power flow controller (UPFC) model based on a modularization multilevel converter (MMC) is composed of a static synchronous series compensator(SSSC) and a parallel static synchronous compensator (STATCOM), on the basis of the switching period average equivalent principle, alternating current side and direct current side equivalent controlled source models of the static synchronous compensator (STATCOM) are built, then, alternating current side and direct current side equivalent controlled source models of the series compensator (SSSC)are built separately, an equivalent capacitor is connected to a direct current bus between the static synchronous series compensator (SSSC) and the static synchronous compensator (STATCOM), and parallel side and series side combined equivalent modeling and simulation calculation of the UPFC is achieved. The dynamic characteristics of subsynchronous oscillation and low-frequency oscillation in a power system of the UPFC can be accurately reflected, the UPFC model is simplified, the calculation speed is increased, and the requirements for stable analysis and control precision of the power systemcan be met.
Owner:GLOBAL ENERGY INTERCONNECTION RES INST CO LTD +2

Three-phase LCL type inverter control method and device based on harmonic interference observer

ActiveCN110635707AImprove output current qualityImprove Steady State Tracking PerformanceAc-dc conversionCapacitanceLow-pass filter
The invention discloses a three-phase LCL type inverter control method and device based on a harmonic interference observer. The method comprises the following steps of establishing a mathematical model under a dq rotating coordinate; introducing capacitive current active feedback damping to obtain an equivalent controlled object mathematical model, and discretizing the model to obtain a z-domainmathematical model; on the basis of proportional negative feedback of a current inner loop and direct feedforward of a power grid voltage, designing a Q (z) filter of a discrete disturbance observer by adopting an infinite impulse response filter method, introducing a first-order low-pass filter and a zero-phase shift low-pass filter into a Gpn-1 (s) channel and an output channel of the disturbance observer to filter a high-frequency noise, and introducing two beats of advance into output of the disturbance observer to compensate time delay of digital control; subtracting an output observationvalue of the disturbance observer from the output of the current inner loop proportional negative feedback, and compensating disturbance so as to obtain a high-quality inverter output current. A problem of LCL inverter output current distortion caused by disturbance of a dead zone effect, power grid voltage distortion, parameter perturbation and the like is solved.
Owner:HUAZHONG UNIV OF SCI & TECH +2

ESO-based magnetic suspension ball sliding mode variable structure control method

The invention relates to an ESO-based magnetic suspension ball sliding mode variable structure control method. The ESO-based magnetic suspension ball sliding mode variable structure control method comprises the following steps that 1, linear treatment is carried out on a mechanism model of a magnetic suspension ball system at the equilibrium point; 2, an expanded state space model of the magneticsuspension ball system is constructed; 3, an ESO for observing and estimating the speed state and unknown disturbance is designed, and disturbance information is used for compensating a controller; 4,the stability of the ESO is determined; 5, an error system of the magnetic suspension ball system is constructed; 6, a sliding mold surface function is designed, and an equivalent control law is solved; and 7, a sliding mode variable structure controller is constructed by using a power approaching law, and a sliding mode control law and a final control law are solved. According to the ESO-based magnetic suspension ball sliding mode variable structure control method, the speed state of small balls and the unknown external disturbance are observed and estimated, the sliding mode variable structure controller is adopted to control the system, a disturbance estimation value serves as the compensation amount of the controller, and the robustness and the anti-interference performance of the system are enhanced.
Owner:ZHEJIANG UNIV OF TECH

Control method of vehicle-mounted flywheel battery radial suspension support system based on working condition

The invention discloses a control method of a vehicle-mounted flywheel battery radial suspension support system based on working conditions. The method includes: 1, taking a magnetic bearing system asa controlled object, and establishing a rotor dynamic model and a system state equation of the magnetic bearing system under different working conditions of the flywheel battery by using a dynamic test and a dynamic simulation; 2, subtracting the output x of the magnetic bear system from the target air gap x* to obtain the air gap error ex, and designing a sliding mode switch surface and a sliding mode controller including an equivalent control and a switching control based on the air gap error ex, a dynamic model and a state equation, and obtaining the sliding mode control law; 3, forming afuzzy RBF neural network by combining fuzzy control and an RBF neural network, and adjusting the constant velocity gain [epsilon] and exponential gain k of switching control by using the fuzzy RBF neural network; 4, adding a current controller, converting the output of the fuzzy sliding mode controller into the given current value of the current inner loop, and controlling the chopper to adjust the magnitude of the control current of the maglev bearing system. The control method improves the transient response rate of the current, and outputs the control current [delta] i of the maglev bearingsystem by the chopper.
Owner:JIANGSU UNIV

Two-dimensional pointing mirror imaging tracking image servo control method

ActiveCN106842911AHigh measurement accuracySolving control problems under uncertaintyAdaptive controlDifferentiatorStator coil
Disclosed is a two-dimensional pointing mirror imaging tracking image servo control method. The two-dimensional pointing mirror imaging tracking image servo control method comprises collecting the azimuth axis angle and the pitch axis angle of a two-dimensional pointing mirror as angle position measurement feedback signals, and collecting the offset of a CCD (charge coupled device) camera focal plane target as image information feedback; calculating increment required by an axis tracking target of the two-dimensional pointing mirror, and establishing a tracking differentiator; simplifying a voice coil motor stator coil model into an RL (resistance-inductance) network, defining axis parameter estimation errors of the two-dimensional pointing mirror, performing computation to obtain speed equivalent control quantity, angular speed tracking errors and axis current equivalent control quantity, and further to obtain the axis voltage control quantity of the two-dimensional pointing mirror to generate driving signals and to complete servo control. The two-dimensional pointing mirror imaging tracking image servo control method is based on image feedback information, thereby, compared with pure two-dimensional pointing mirror angle position servo control, adding image feedback information, improving the measuring precision and having the advantage of high control precision.
Owner:BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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