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559results about How to "Achieve compensation" patented technology

Control method and control system for worming torque of electric automobile and electric automobile

The invention discloses a control method and a control system for a worming torque of an electric automobile. The control method comprises the following steps: acquiring a basic part T1 of the worming torque according to a vehicle speed u look-up table; calculating a gravity acceleration component a3 of a vehicle according to a longitudinal acceleration a1 and a travel acceleration a2 of the vehicle; calculating a gradient resistance compensation part initial value T2' of the worming torque according to a complete vehicle mass m, the gravity acceleration component a3 and a tire rolling radius R; attenuating the obtained gradient resistance compensation part initial value T2' of the worming torque with increase of the vehicle speed according to a current vehicle speed u, thereby obtaining a gradient resistance compensation part T2 of the worming torque; adding the basic part T1 of the worming torque with the gradient resistance compensation part T2 of the worming torque to obtain a total worming torque T; and controlling a driving motor to output the total worming torque T to enable the vehicle to worm. The control method and the control system take a road grade into consideration to achieve compensation of gradient resistance, thereby enabling the vehicle to have same acceleration performance and good comfort no matter traveling uphill, downhill or on a level road.
Owner:ZHEJIANG GEELY HLDG GRP CO LTD +1

Airborne laser radar pitch angle deviation real-time compensation method and device

The invention discloses an airborne laser radar pitch angle deviation real-time compensation method and an airborne laser radar pitch angle deviation real-time compensation device. The device comprises a laser scanner device capable of realizing pitch angle deviation compensation, a pitch angle compensation controller and driving device, a GPS/INS combined measurement device, wherein the laser scanner device capable of realizing the pitch angle deviation compensation comprises a laser scanning transmitting and receiving system, a scanning prism, a compensation mirror, a photoelectric axial angle encoder and a compensation mirror motor; the GPS/INS combined measurement device acquires the attitude angle (pitch angle, rolling angle and yaw angle) deviation of a airborne platform and provides the acquired attitude angle deviation to the pitch angle compensation controller and driving device; and the pitch angle compensation controller and driving device controls the motor of the compensation mirror by using a compensation signal, receives a feedback signal from the compensation mirror photoelectric angle encoder, completes the closed-loop control of the pitch angle deviation compensation mirror and realizes the real-time high-accuracy compensation of the pitch angle deviation of an airborne laser radar.
Owner:BEIHANG UNIV

Three-level inverter dead time compensation control method

InactiveCN103236798AImproved output current waveformActual output line voltage risesAc-dc conversionThree levelVoltage vector
A three-level inverter dead time compensation control method is used for compensating the decrease of system performance caused by dead time. According to the topological structure of a three-phase three-level PWM (pulse width modulation) inverter, the method first sets corresponding dead time and determines the on-off delays of power elements in the inverter; the method then considers the tube voltage drops of the power transistors of the inverter and the tube voltage drops of clamping diodes of the inverter and calculates the common voltage expression of the output neutral point of the inverter; afterwards, according to the sector with three-phase current value and a reference voltage vector, the method determines the relational coefficient between voltage error caused by the tube voltage drops of the power transistors, the tube voltage drops of the clamping diodes and the on-off delays of the power transistors and current, and thereby the total dead time compensation time of each phase of the three-level PWM inverter is worked out. The method takes the dead time, the on-off delays of the power elements and the tube voltage drops into full consideration, solves the problem of voltage and current distortion caused by the dead time effect in the three-level inverter, and enhances system performance.
Owner:NORTH CHINA UNIVERSITY OF TECHNOLOGY

Reactive power compensation device based on novel modular multilevel topology and control method thereof

A reactive power compensation device based on novel modular multilevel topology and a control method thereof relate to a high-voltage and large-power reactive power compensation device. In the prior art, compensation in a high-voltage and large-power field is limited and an inhibiting ability to circulation is insufficient. The invention aims at solving the above problems. A three-phase alternating-current power supply, a resistance-inductance load, a MMC converter, a signal detection circuit, a control circuit and a driving circuit are included. The MMC converter comprises three bridge arms which share a same structure and are connected in parallel. Each bridge arm comprises an upper bridge arm and a lower bridge arm which are symmetrical about a middle point of the bridge arm and are connected in series. Each upper bridge arm comprises a resistor, an inductor, several half-bridge units and an H bridge unit which are connected in series. The inductor of each upper bridge arm and an inductor of each lower bridge arm are connected in series. The middle points of the three bridge arms of the converter are connected in parallel between the three-phase alternating-current power supply and the load through a lead. By using the device and the method in the invention, power-grid reactive power can be compensated; a three-phase imbalance problem of a system is solved; effects of supporting a power grid voltage and inhibiting the circulation are achieved.
Owner:HARBIN UNIV OF SCI & TECH

Self-force-increasing type electronic-mechanic brake for automobile

The invention discloses a self-force-increasing type electronic-mechanic brake for an automobile. An upper friction plate and a lower friction plate are arranged at the two sides of a brake disc. The upper friction plate is fixedly mounted on a brake caliper body. The brake caliper body is mounted on a brake caliper bracket through guiding rods and can move axially on the guiding rods. A dust cover is arranged between the brake caliper body and each guiding rod. A first motor is fixed to a lower wedge block through first screws. The first motor is connected with a first threaded rod through a first coupling. The first threaded rod is in transmission connection with a push rod through a thread. In the braking process, the first motor drives the first threaded rod to rotate, the first threaded rod pushes the push rod to move in the horizontal direction, and furthermore, the push rod pushes an upper wedge block to move in the horizontal direction and the vertical direction; normal brake clearances are eliminated; and the lower friction plate is in contact with the brake disc, and braking is achieved. The self-force-increasing type electronic-mechanic brake for the automobile has the self-force-increasing function; the input torque of each motor can be greatly reduced; and meanwhile, the self-force-increasing type electronic-mechanic brake has the function that the clearance can be adjusted automatically, and wear of the friction plates is compensated.
Owner:JINHUA VOCATIONAL TECH COLLEGE

Nonlinear system active disturbance rejection control method based on interference observer

ActiveCN107168071AAchieving Simultaneous EstimationAchieve compensationAdaptive controlInterference resistanceHarmonic
The invention relates to a nonlinear system active disturbance rejection control method based on an interference observer, targeting a nonlinear single-input and single-output system containing an unknown nonlinear function and harmonic wave interference. The nonlinear system active disturbance rejection control method based on an interference observer comprises steps of performing mathematic representation on the harmonic wave interference and the nonlinear function, establishing an external model of the harmonic wave interference, designing an interference observer and an extended state observer on the basis of control input and measurement output information, completing estimation on the harmonic wave interference, the unknown non-linear function and a system state, designing an active disturbance controller according to the output of the interference observer and the extended state observer and completing gain solving of the observer and the controller on the basis of a separation theorem and a pole arrangement theory. The nonlinear system active disturbance rejection control method based on the interference observer has advantages of high interference resistance and high control accuracy and can be used for high accuracy control containing the interference and the unknown non-linear system.
Owner:BEIHANG UNIV

Multi-agent fully-distributed active disturbance rejection time-varying formation control method

ActiveCN110597061AReduce the risk of jitterHelps smooth changesAdaptive controlDifferentiatorMulti-agent system
The invention discloses a multi-agent fully-distributed active disturbance rejection time-varying formation control method. The multi-agent fully-distributed active disturbance rejection time-varyingformation control method is based on a multi-agent system which is composed of N autonomous second-order isomorphic agents. The multi-agent fully-distributed active disturbance rejection time-varyingformation control method uses an active disturbance rejection control idea for reference, and comprises the steps of: firstly, constructing an active disturbance rejection time-varying formation controller and an action weight self-adaptive updating law based on a self-adaptive control and error feedback control strategy according to interaction weights and formation state errors of the agents; adopting an extended state observer to determine disturbance compensation; adopting a tracking differentiator to generate a time-varying formation instruction; further providing a completely distributedcontrol gain design method; and finally providing the multi-agent fully-distributed active disturbance rejection time-varying formation control method. The multi-agent fully-distributed active disturbance rejection time-varying formation control method realizes the effect of how to implement active disturbance rejection time-varying formation control on the multi-agent system affected by externaldisturbance in a completely distributed manner, so that the multi-agent system has disturbance suppression robustness while realizing time-varying formation.
Owner:ROCKET FORCE UNIV OF ENG

Gain-and-direction-orientated structure thermal deformation compensation method for satellite-borne active phase control array antenna

The invention discloses a gain-and-direction-orientated structure thermal deformation compensation method for a satellite-borne active phase control array antenna. The method comprises the steps of determining structural parameters, material attributes and electromagnetic parameters of the antenna; determining antenna environment thermal load; calculating antenna temperature field distribution under sunshine; determining T/R assembly thermal power consumption; calculating antenna temperature field distribution under the T/R assembly thermal power consumption; performing temperature field superposition and calculating the thermal deformation of the antenna structure; extracting position offset in the array element geometric center; calculating the additional error of the array element space phase; determining the amplitude and phase distribution of array element excitation current; calculating the electrical performance of the antenna; judging whether gain and direction are both satisfied simultaneously or not; and calculating the antenna ideal main beam directed unit vector, the adjusting amount of the array element space phase, and the phase current of the compensated array element excitation current. The compensation method provided by the invention is combined with a phase adjusting method, so that the electrical performance compensation to the deformed satellite-borne active phase control array antenna is realized; the problem of antenna electrical performance degradation caused by structural thermal deformation is solved; and the normal operation of the antenna can be ensured.
Owner:XIDIAN UNIV

Carrier wave frequency offset compensation method, apparatus and receiving system

A carrier wave frequency offset compensation method, an apparatus and a receiving system are disclosed. The carrier wave frequency offset compensation method comprises the following steps of aiming at each sweeping frequency point in a sweeping frequency scope, calculating a signal intensity indication value of a receiving signal respectively, wherein the sweeping frequency point is used for adjusting a frequency of a receiving-end local oscillator signal; based on the signal intensity indication value and a frequency value of each corresponding sweeping frequency point, determining an estimation value of the carrier wave frequency offset; based on the estimation value of the carrier wave frequency offset, adjusting the frequency of the local oscillator signal so as to realize compensation to the carrier wave frequency offset. Further, through a fine compensation method of the carrier wave frequency offset, the fine compensation is performed on the carrier wave frequency offset after the compensation. Under the condition that the carrier wave frequency offset is large, estimation and compensation can be performed on the carrier wave frequency offset effectively. Under a small bandwidth work mode of a low pass filter, the large carrier wave frequency offset can be compensated. Receiver performance is increased and simultaneously a carrier wave frequency offset compensation scope can be effectively expanded.
Owner:SHANGHAI EASTSOFT MICROELECTRONICS

Digital communication system and method for improving flatness in signal band thereof

The invention relates to the field of digital signal processing of wireless communication and provides a digital communication system, which comprises an analog receiving module which carries out analog filtering and analog down-conversion processing on radio frequency signals, a digital down-conversion module which carries out decimation filtering processing on digital signals, a pass band compensation module which carries out fluctuating compensation on signals in pass bands, a digital up-conversion module which carries out interpolation filtering and up-conversion frequency mixing processing on the digital signals and an analog launching module which carries out analog filtering and analog up-conversion processing on the radio frequency signals. The invention also provides a method for improving flatness in a signal band in the digital communication system. A frequency domain compensation coefficient is obtained by the digital filtering processing in the frequency domain, namely testing the fluctuation characteristics of the system, and frequency domain filtering processing is carried out on the frequency domain signals according to the frequency domain compensation coefficient, thus realizing fluctuation correction and compensation in the signal band and improving the flatness in each carrier signal pass band in a digital repeater system.
Owner:COMBA TELECOM SYST CHINA LTD

Error calibration compensation method of accelerometers in MEMS-IMU under dynamic environment

The invention discloses an error calibration compensation method of three axial accelerometers in an MEMS-IMU under the dynamic environment. The error calibration compensation method includes the steps of enabling an outer frame of a rotary table to operate in a speed mode, then enabling the Z axis to return to the zero position, enabling an inner frame of the rotary table to operate in a sine mode, changing installation of the IMU, respectively enabling the direction of a sensitive shaft of the X-axis accelerometer and the direction of a sensitive shaft of the Y-axis accelerometer to be parallel to the sky direction, enabling the accelerometers to sense the dynamic accelerated speeds and the dynamic angle speeds in the operating mode same as that of the Z-axis accelerometer, recording the output data of the three axial accelerometers, carrying out analysis and processing, and obtaining the installing errors, the calibration coefficients and the zero wanders of the three axial accelerometers in the MEMS-IMU and influence factors of the dynamic angle speeds on the accelerometers. The error calibration compensation method is simple and easy to implement, obviously improves the accuracy of an MEMS-IMU system, and is particularly suitable for systems with low-cost and low-accuracy MEMS accelerometers.
Owner:SOUTHEAST UNIV
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