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53results about How to "Avoid nonlinearity" patented technology

Method for measuring electro-optic phase modulator modulation factor

ActiveCN103926059AAvoid nonlinear processAvoiding Linewidth and Phase Noise IssuesTesting optical propertiesPhysicsVIT signals
The invention discloses a method for measuring an electro-optic phase modulator modulation factor, and relates to the technical field of the photoelectronic technique. In order to solve the problems that phase modulation signals cannot be directly detected on a photoelectric detector and nonlinearity cannot be omitted in PM-IM and FM-IM conversion processes, an optical fiber interferometer is adopted as a measuring device and composed of a beam splitter, an electro-optic phase modulator to be measured, an acousto-optic frequency shifter, an auxiliary electro-optic phase modulator and a beam combiner, wherein the electro-optic phase modulator to be measured is arranged on one interference arm of the optical fiber interferometer, the acousto-optic frequency shifter and the auxiliary electro-optic phase modulator are placed on the other interference arm of the optical fiber interferometer, and sinusoidal signals with different frequencies are loaded to the electro-optic phase modulator to be measured, the acousto-optic frequency shifter and the auxiliary electro-optic phase modulator respectively. Frequency response of the photoelectric detector is eliminated by setting a frequency relation of the loaded sinusoidal signals, self-calibration measurement is achieved, measuring accuracy of the electro-optic phase modulator modulation factor is improved, and the method has good application value.
Owner:UNIV OF ELECTRONIC SCI & TECH OF CHINA

Fiber-optic compensation for dispersion, gain tilt, and band pump nonlinearity

An apparatus and method are described for combining optical amplification and dispersion compensation in a Raman amplifier. A Dispersion-Managing Raman Amplifier (DMRA) combines Raman amplification with dispersion compensation by selecting the length and dispersion of the gain fiber to balance the dispersion of the link. This gain fiber is also single-mode at the signal and pump wavelengths. The pumping level is adjusted to balance the losses from the gain fiber and transmission link, while the pumping configuration is selected to remain within the 3 dB loss length for the pumping light. When the amplifier is split into two segments, the two segments may be joined by an isolator, a gain equalization element, and/or an optical add/drop multiplexer. For WDM transmission systems based on dispersion-shifted fiber (DSF), operation in the “violet band” between 1430–1530 nm is based on Raman amplification. By using a DMRA, a dispersion and nonlinearity managed system can be implemented. In particular, 4WM does not phase match in such a system, and modulation instability is absent in the transmission link. Furthermore, gain equalization can be added to the DMRA by cascading one or two Mach-Zehnder frequency filters. The invention also includes a method for symmetrically adding channels below and above the C-band, the gain tilt within the C-band can be minimized. Therefore, a roughly equal number of channels should be placed in the short-wavelength S-band and the long-wavelength L-band to minimize the Raman energy exchange in the C-band. Also, whereas C- and L-bands can be amplified using erbium-doped fiber amplifiers, the S-band can use either discrete or distributed Raman amplifiers. To minimize the interaction between pumps for different bands, alternate band pumps can be spatially dispersed and/or cross-polarized. The distributed Raman amplification can be achieved by pumping the transmission line with discrete laser diodes or by a Raman oscillator.
Owner:NEPTUNE SUBSEA IP LTD +1

Quick initial alignment method for moving base of SINS (strapdown inertial navigation system) based on lie group description

The invention discloses a quick initial alignment method for a moving base of an SINS (strapdown inertial navigation system) based on lie group description. The method comprises the following steps: replacing traditional quaternion description with lie group description to realize calculation of SINS attitude transformation; establishing a linear initial alignment model by using a lie group differential equation; establishing an augmented initial alignment model by taking gyroscopic drift as an augmented state quantity; and then realizing synchronous estimation of an initial attitude matrix and gyroscope constant drift by adopting a matrix-form Kalman filtering algorithm. According to the quick initial alignment method, the gyroscope constant drift is taken as the augmented quantity, and compared with a traditional initial alignment model, a more accurate augmented linear alignment model is established. The alignment method disclosed by the invention can realize one-step direct alignment of the SINS, greatly shortens the alignment time, is convenient for compensating errors in a strapdown resolving process, effectively improves the alignment precision, and is more suitable for practical engineering application.
Owner:BEIJING UNIV OF TECH

Prediction method for high-cycle fatigue life of single crystal air film hole member

The invention provides a prediction method for high-cycle fatigue life of a single crystal air film hole member, and relates to the technical field of porous mediums. The method comprises the steps ofdetermining a dangerous path according to a hole distribution mode of the single crystal air film hole member; building a crystal plasticity theory model, and inputting related parameters of the crystal plasticity theory model to a finite element model; outputting stress distribution of the dangerous path through the finite element model, and obtaining a maximum main stress amplitude and a maximum resolved shear stress amplitude on the dangerous path; and building a critical distance model, determining parameters of the critical distance model according to the maximum main stress amplitude and the maximum resolved shear stress amplitude, and performing calculation by an iterative program to obtain the high-cycle fatigue life of the single crystal air film hole member. According to the method, anisotropic material properties of single crystal and a deformation mechanism of crystal slip are considered; the difficult problem of high-cycle fatigue damage nonlinearity is solved; and a prediction result is small in dispersity and high in precision.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Sigma-delta PLL frequency measuring circuit and method

The invention provides a sigma-delta PLL frequency measuring circuit and method. The circuit comprises a rectifying circuit, a phase discriminator, a loop filter, an ADC and a delay link which are sequentially arranged from the input end. The output end of the delay link is fed back and input to the phase discriminator through a counter. The frequency measuring method comprises the steps that after the rectifying circuit filters and amplifies a signal to be detected, the signal to be detected is converted into a square signal with the frequency same as that of the signal to be detected; the phase discriminator measures the zero crossing point time difference of the square signal and an output signal of the counter, and a pulse current signal with the output area and the time in a direct proportion; after the integration and the filtering are carried out on an output current of the phase discriminator through the loop filter, the output current is converted into a voltage signal; the ADC converts analog voltage output by the loop filter into a digital signal; the delay link delays the digital signal output by the ADC, and therefore the frequency of the signal to be detected is determined; a counter output signal with the clock period and the delayed digital signal in a direct proportion is generated by the counter, and is output to the phase discriminator. The anti-noise capacity is strong in the process of measuring the frequency, the resolution ratio is high, and the frequency measurement can be achieved easily.
Owner:NANJING UNIV OF SCI & TECH

Large-flow high-stability Mach number wind tunnel rapid adjusting system and method based on temporary charging air source

The invention provides a large-flow high-stability Mach number wind tunnel rapid adjusting system and method based on a temporary charging air source. The large-flow high-stability Mach number wind tunnel rapid adjusting system structurally comprises a temporary charging air source, a main valve, an auxiliary valve, a spraying pipe, a pressure sensor, a Mach number sensor and a control unit, and the auxiliary valve has the faster small-flow adjusting capacity and is connected with the main valve in parallel. The method comprises the following steps: (1) on the basis of 50% opening degree of an auxiliary valve, carrying out main valve manual adjustment on a characteristic Mach number point in a wind tunnel capability range to obtain a main valve opening degree and air source pressure relation curve cluster under a corresponding Mach number; (2) according to the instruction Mach number and the current air source pressure, obtaining the opening degree of a main valve through two-dimensional linear interpolation; and (3) carrying out closed-loop PID adjustment of the instruction Mach number by using the auxiliary valve, and maintaining the outlet Mach number. According to the invention, a composite control strategy of main valve feedforward and auxiliary valve closed-loop PID is adopted, and the problem that an outlet Mach number is not easy to stabilize due to continuous decrease of gas source pressure, poor repeatability of a main valve, strong nonlinearity and slow adjusting speed in a wind tunnel test is solved.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Strapdown inertial navigation system (SINS) swinging base self-aligning method based on Lie group optimal estimation

The invention discloses a strapdown inertial navigation system (SINS) swinging base self-aligning method based on Lie group optimal estimation. Lie group description is adopted instead of traditionalquaternion description to realize the calculation of SINS attitude transformation; a linear initial self-aligning filtering model based on the Lie group description is established by using a Lie groupdifferential equation; and a Lie group optimal estimation method is designed to determine an initial attitude matrix required by navigation. According to the method, the optimal estimation is directly performed on the initial attitude matrix by a Lie group optimal estimation algorithm, so that the initial attitude estimation problem is transformed into the optimal estimation problem of a SO(3) group; one-step direct self-alignment of the SINS is realized; the aligning time is shortened greatly; the problems of non-uniqueness and non-linearity generated by the traditional quaternion description of the initial attitude matrix are solved; the alignment accuracy is improved effectively; and the problem that the orthogonality of a rotation matrix cannot be ensured due to the additivity error and the calculation error in a Lie group filtering method is solved. The method has practical value in the practical engineering.
Owner:BEIJING UNIV OF TECH

Bi-directional optical-amplifier module

Disclosed is a bi-directional optical-amplifier module including first through fourth optical amplifiers, a mid-stage device for performing a desired signal processing for an upward or downward optical signal passing therethrough, a first optical-signal-path-setting device for supplying an optical signal inputted to a first input/output terminal of the bi-directional optical-amplifier module while outputting an optical signal outputted from the fourth optical amplifier to the first input/output terminal, a second optical-signal-path-setting device for supplying an optical signal inputted to a second input/output terminal of the bi-directional optical-amplifier module while outputting an optical signal outputted from the third optical amplifier to the second input/output terminal, a third optical-signal-path-setting device for outputting an optical signal outputted from the first optical amplifier to a first input/output terminal of the mid-stage device while supplying an optical signal outputted from the first input/output terminal of the mid-stage device to the fourth optical amplifier, and a fourth optical-signal-path-setting device for outputting an optical signal outputted from the second optical amplifier to a second input/output terminal of the mid-stage device while supplying an optical signal outputted from the second input/output terminal of the mid-stage device to the third optical amplifier.
Owner:SAMSUNG ELECTRONICS CO LTD

Low-voltage compensation device and method of energy-saving power distribution network

ActiveCN108173270ASolve low voltageSolve the problem that the access point voltage is too low while runningSingle network parallel feeding arrangementsAc network voltage adjustmentLow voltageFilter capacitor
The invention discloses a low-voltage compensation device and method of an energy-saving power distribution network. The device is divided into a rectification part, an inversion part and a bypass unit, wherein the rectification part comprises a relay QF1, a filtering capacitor C1, an AC reactor L1, an IGBT tube G1, a rectification diode and a photovoltaic cell panel, the inversion part comprisesa relay QF2, an IGBT tube G2, an IGBT tube G3, an inversion inductor L2 and a filtering capacitor C2, and the bypass unit comprises a bidirectional thyristor SCR. With the adoption of a series voltagecompensation mode, the problem of low voltage of the power distribution network is solved, and the device only needs to provide a part of load power; with the adoption of a transformerless DC seriesmode, the problems of loss and non-linearity of the transformer are prevented; combined with photovoltaic power generation, a working mode is switched, and the problem of extremely low voltage of a plurality of voltage regulation devices simultaneously running at access points is solved; and meanwhile, photovoltaic power generation is fully utilized, the effect of energy saving and emission reduction is achieved.
Owner:西安翌飞核能装备股份有限公司

SINS strapdown inertial navigation system shaking base self-alignment method based on Lie group optimal estimation

The invention discloses an SINS strapdown inertial navigation system shaking base self-alignment method based on Lie group optimal estimation, which adopts Lie group description to replace traditionalquaternion description to realize calculation of SINS attitude transformation, and utilizes a Lie group differential equation to establish a linear initial alignment filtering model based on the Liegroup description. And performing equivalent transformation on the state-related error by utilizing the left multiplication invariance of the plum group and the exponential mapping between the plum group and the plum algebra, establishing an equivalent state-independent plum algebra filtering equation, and estimating the initial attitude through the equivalent equation. According to the method, the state-dependent noise under the Lie group model is equivalent to the state-independent noise under the Lie algebra, compared with a traditional Lie group model, a more accurate Lie group linear alignment model is established, and the problems of non-uniqueness and nonlinearity caused by the fact that a traditional quaternion describes an initial attitude matrix are avoided. The method greatly shortens the alignment time, effectively improves the alignment precision, and is more suitable for practical engineering application.
Owner:BEIJING UNIV OF TECH

Movement implementing mechanism for LAMOST type astronomical focus panel

An LAMOST astronomical telescope focal panel movement realizing mechanism is characterized in that a rotary movement mechanism, a tilted movement mechanism and a focusing movement mechanism are set as a co-movement mechanism, wherein, a large gear and a circular guide rail are fixedly connected on a base; six matched slide blocks are distributed on the circular guide rail; the slide blocks are connected with pinions through connecting plates; each pinion is meshed with the large gear; a drive motor is arranged on a shaft; the slide blocks are respectively connected with supporting rods through left single rod joint bearings; each supporting rod is connected on a focal panel through a right single rod joint bearing; every two supporting rods are arranged as one group in a V-shaped form, and one end of each of the two supporting rods leans against the connecting points of the focal panel through the right single rod joint bearings; three groups of connecting points are distributed in the same circle on the focal panel by 120 degrees; and the other end of each of the two supporting rods has a certain distance through the locations of the two slide blocks connected with the left single rod joint bearing on the circular guide rail. The invention not only simplifies the mechanical structure and the control system, but also improves the stability of the system.
Owner:NANJING INST OF ASTRONOMICAL OPTICS & TECH NAT ASTRONOMICAL OBSE
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