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268 results about "Zero bias" patented technology

Zero bias. [′zir·ō ′bī·əs] (electronics) The condition in which the control grid and cathode of an electron tube are at the same direct-current voltage.

Method for determining driving state of vehicle based on acceleration sensor

ActiveCN102167041APrevent dangerous driving behaviorEnsure driving safetyDriver/operatorOriginal data
The invention discloses a method for determining the driving state of a vehicle based on an acceleration sensor. The method comprises the following steps of: A, acquiring the longitudinal acceleration, the transverse acceleration and the vertical acceleration of an automobile by using a three-axial acceleration sensor; B, calculating a conversion matrix of an automobile coordinate system and an acceleration sensor coordinate system, acquiring the initial attitude of the acceleration sensor, namely the initial angle between the acceleration sensor and the automobile, and performing zero bias filtering processing on the acquired accelerations so as to acquire the acceleration value of the automobile coordinate system; and C, determining the driving state of the vehicle according to the acceleration values of a plurality of continuous automobile coordinate systems. In the method for determining the driving state of the vehicle based on the acceleration sensor, the original data is acquired by the acceleration sensor, and the driving state of the vehicle is determined by analyzing and processing three axial accelerations, so that the driving behaviors and the driving state of a driver are known, vehicle managers are assisted in normalizing the driving behaviors, dangerous driving behaviors are prevented, and driving safety is ensured.
Owner:SHENZHEN CASTEL WIRELESS TELECOMM

Capacitance testing circuit and capacitance-type sensor interface circuit chip thereof

The invention discloses a capacitance testing circuit and capacitance-type sensor interface circuit chip thereof, which relates to the sensor device field and resolves problems that the capacitance testing circuit has complicated structure and the capacitance-type sensor interface circuit chip has large volume and is inefficient. The capacitance testing circuit includes a capacitance readout front end circuit, a demodulation amplifying circuit whose input end is connected to the capacitance readout front end circuit, and a buffering amplifying circuit whose input end is connected to the demodulation amplifying circuit. The capacitance-type sensor interface circuit chip includes a self measuring circuit, a bias current producing circuit, a sensor zero bias compensating circuit, a reference voltage generation circuit, a clock generation circuit, and a capacitance testing circuit respectively connected to the circuits; the self measuring circuit and the sensor zero bias compensating circuit are respectively connected to a outer capacity sensor; the capacitance-type sensor interface circuit chip is prepared by using an integrate circuit technique. The invention is suitable for open-loop or equilibrium closed-loop accelerameter and vibratory rate gyroscope.
Owner:TSINGHUA UNIV

MEMS accelerometer with temperature compensation function

The invention relates to an MEMS accelerometer with the temperature compensation function. The MEMS accelerometer with the temperature compensation function comprises an acceleration sensor, a temperature sensor and a temperature compensation chip, wherein the acceleration sensor and the temperature sensor are connected with the temperature compensation chip. A temperature compensation method adopted by the temperature compensation chip comprises the steps that (1), zero biases and a set of output values of a scale factor are measured under a plurality of temperature points, the zero biases and the output values are fitted to be a fitting surface, and a series of fitting coefficients are obtained and arranged to be a coefficient matrix; (2), modeling is carried out on output signals of the acceleration sensor and the output signals of the temperature sensor so as to be expressed as a model matrix; (3), dot product is carried out on the coefficient matrix and the model matrix so as to obtain an output formula after the acceleration sensor obtains the temperature compensation; (4), the fitting coefficients and the output formula are written into the temperature compensation chip to be calculated. Through three-dimensional fitting of the surface and compensation after calculation, influence on a system from errors generated when the accelerometer is assembled and installed is reduced effectively.
Owner:EAST CHINA INST OF OPTOELECTRONICS INTEGRATEDDEVICE

MEMS (micro-electro-mechanical system) fully decoupled closed-loop gyroscope

PendingCN108507555AImprove partial stability indexGood ability to resist cross error interferenceSpeed measurement using gyroscopic effectsGyroscopes/turn-sensitive devicesStability indexClosed loop
The invention discloses a MEMS (micro-electro-mechanical system) fully decoupled closed-loop gyroscope. The gyroscope comprises a substrate and a sensitive device layer, wherein an insulating layer isarranged between the substrate and the sensitive device layer; the sensitive device layer comprises a first substructure, a second substructure and a coupling connection beam; each of the first substructure and the second substructure comprises a driving frame, driving folding beams, driving decoupling beams, a Coriolis mass block, a detection frame, detection beams, detection decoupling beams, driving fixed comb teeth, driving movable comb teeth, driving detection fixed comb teeth, driving detection movable comb teeth, detection fixed comb teeth, detection movable comb teeth, force feedbackfixed comb teeth, force feedback movable comb teeth and anchor points. Generation of quadrature error signals is suppressed, and the zero bias stability index of the MEMS gyroscope is improved; the gyroscope has compact structure and small chip area, and can prevent a detection-mode sensitive mass from twisting due to larger displacement, thereby having good overall linearity and high measurementaccuracy.
Owner:四川知微传感技术有限公司

Vibration waveform controlling system of electro-hydraulic exciter

The invention relates to a vibration waveform controlling system of an electro-hydraulic exciter, which comprises an oil source, a high-frequency excitation valve, a parallel servo valve, a hydraulic actuator and a loading object, wherein the parallel servo valve comprises a zero-bias servo motor; the high-frequency excitation valve is a 2D electro-hydraulic high-frequency excitation valve which comprises an axial servo motor; the vibration waveform controlling system also comprises a position detection device, a data acquisition controller, an electro-hydraulic servo controller and an industrial personal computer; the electro-hydraulic servo controller is connected with the zero-bias servo motor and the axial servo motor; and the industrial personal computer comprises a control execution module for decomposing a set excitation waveform signal into a zero-bias control signal and an amplitude value control signal and outputting the control signals to the electro-hydraulic servo controller, and a feedback comparison module for comparing a zero-bias feedback signal and an amplitude value feedback signal with the zero-bias control signal and the amplitude value control signal respectively and sending a compared differential value signal to the electro-hydraulic servo controller. The vibration waveform controlling system adopts closed-loop control, has small distortion degree of output waveform and high controlling precision.
Owner:ZHEJIANG UNIV OF TECH

Single-axle table calibration method for fiber optic gyro strapdown inertial navigation system

The invention aims at providing a single-axle table calibration method for a fiber optic gyro strapdown inertial navigation system. The fiber optic gyro strapdown inertial navigation system is placed on a single-axle table, the fiber optic gyro strapdown inertial navigation system is electrified for preheating, the angular velocity outputted by a fiber optic gyro and the specific force outputted by a quartz flexible accelerometer are collected, then the single-axle table is controlled to rotate at 90 degrees counter-clockwise around a rotating shaft three times, the angular velocity outputted by the fiber optic gyro and the specific force outputted by the quartz flexible accelerometer at each time are respectively collected, and the drift of the fiber optic gyro in an x, y and z-axis coordinate system of an inertia device and the zero bias value of the quartz flexible accelerometer in the x, y and z-axis coordinate system of the inertia device are further obtained. The method can measure the drift of the fiber optic gyro and the zero bias value of the quartz flexible accelerometer by utilizing the single-axle table to rotate into different angular positions; furthermore, the calibration cost of the single-axle table is low, the steps are simple, and the single-axle table only needs to be placed on the ground during the calibration without a laboratory.
Owner:HARBIN ENG UNIV

Polarization-maintaining photonic crystal fiber gyroscope and manufacturing method thereof

The invention discloses a polarization-maintaining photonic crystal fiber gyroscope light path. The polarization-maintaining photonic crystal fiber gyroscope light path comprises a polarization-maintaining fiber coupler, a broad band optical source, a Y waveguide, a polarization-maintaining photonic crystal fiber ring spliced with a Y waveguide output tail fiber and a detector and is characterized in that the polarization-maintaining fiber coupler acts on a polarization-maintaining fiber fast axis, a Y waveguide tail fiber is a stress birefringence polarization-maintaining fiber, 0-degree axis alignment splicing is performed between the fiber fast axis and the Y waveguide TE mode, the polarization-maintaining pohotonic crystal fiber ring is obtained by winding double macropore type polarization-maintaining photonic crystal fibers, 90-degree axis alignment splicing is performed between the axial direction of double macropore type polarization-maintaining photonic crystal fibers and the axial direction of the stress birefringence polarization-maintaining fiber, and useful signals in the gyroscope light path are all transmitted in the fast axis. The photonic crystal fiber gyroscope light path has the advantages of low temperature sensitiveness, radiation resistance and the like of a common photonic crystal fiber gyroscope, further effectively inhibits polarization errors of the gyroscope and facilitates improvement of zero-bias stability of the fiber gyroscope.
Owner:HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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