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561 results about "Zero phase" patented technology

Phased array antenna having integral calibration network and method for measuring calibration ratio thereof

ActiveUS20110122016A1Calibration expensive and complexCost-effectiveWave based measurement systemsAntennasPhase differenceZero phase
A phased antenna arrangement and a method for estimating the calibration ratio of an active phased antenna having a plurality of phased array antenna elements are described. The phased antenna arrangement includes a plurality of antenna elements, a plurality of receiving channels, an injection unit for injection of calibrating signals into the receiving channels, a point RF-source, located in a far field zone, a distance measurement unit, an amplitude and phase measurement unit and a data processing unit. The method comprises injecting an internal calibrating signal having a known amplitude and phase to each antenna element. An external calibration signal from a stationary RF-source is sequentially injected to all of the phased array antenna elements so that different phases of the external calibration signal arrive at each of the antenna elements. The differences in phases of the external calibration signal reaching the antenna elements are compensated so as compute an effective signal amplitude that would reach all of the antenna elements at zero phase difference. Calibration ratio is calculated as the ratio between the amplitude of the internal calibrating signal to the effective signal amplitude of the external calibration signal.
Owner:ELTA SYST LTD

Failure line selection method of small current ground system by using simulation after zero mode current measure

InactiveCN101242097AOvercome the influence of small fault transient currentRealize correct line selectionEmergency protective circuit arrangementsCapacitanceEngineering
The invention provides a fault route-selecting method by using small current grounding system simulated by measured zero-mode current. The method includes following steps: when a generatrix zero-mode voltage instantaneous value is over the limit, a fault route-selecting is started and recorded immediately; zero-phase shift digital wave filter is used to obtain a high-frequency transient weight of each feed line zero-mode current; orderly the feed line is supposed to be fault feed line, the rest of the high-frequency transient weight of the feed line zero-mode current is quantificationally solved by using the measured simulative method according to the supposed high-frequency transient weight of the feed line zero-mode current and each feed line zero-order distributing capacitance parameter; the actual-measured wave shape and simulative wave shape of the high-frequency transient weight of the feed line zero-mode current are analyzed and a average relative coefficient of the actual-measured wave shape and simulative wave shape of the high-frequency transient weight of the feed line zero-mode current are solved, the route-selecting criterion is formed to achieve the fault route selection. The principle analysis and simulation indicate that route selection of this method is accurate and reliable.
Owner:KUNMING UNIV OF SCI & TECH

Non-destructive detection method of pulse-excited infrared thermal wave phase of fixed viewing field

The invention relates to a non-destructive detection method of pulse-excited infrared thermal wave phase of a fixed viewing field. The non-destructive detection method comprises the following steps: comprehensively applying a multiple-modulation Zoom-FFT refining spectrum method, a thermal-wave data fitting extension method and a zero-phase digital filter method, and carrying out high-accuracy spectral analysis on acquired continuous equally-spaced infrared thermal-wave image sequences before and after thermal excitation, thus quickly obtaining precise ultralow-frequency thermal-image phase diagram and amplitude diagram, and further realizing detection and recognition for defects or damages of equipment. Compared with the prior art, the non-destructive detection method has the beneficial effects that not only can the acquisition frequency, the acquisition time, the acquisition frame number and the refining degree of analysis of thermal images be flexibly set, but also the detection speed, the refining degree and the precision degree can be increased by ten times respectively, the multiplied increase of the detection effect and the detection depth of the defects also can be realized, simultaneously the requirement for computer hardware is also reduced, so that the method is flexible in use, is especially suitable for non-destructive detection of the infrared thermal wave on site and has a wide application prospect.
Owner:PLA SECOND ARTILLERY ENGINEERING UNIVERSITY

Time-frequency synchronization joint estimation method based on multi-carrier receiver of digital television media broadcast (DTMB) system

The invention relates to a time-frequency synchronization joint estimation method based on a multi-carrier receiver of a digital television media broadcast (DTMB) system. The method is characterized by comprising the following steps: step 1, carrying out frame header mode recognition and frame header position coarse estimation; step 2, generating a pseudorandom noise (PN) sequence A of a zero phase matched with the frame header mode by a local PN generator, and carrying out carrier frequency offset estimation by utilizing a step-variable frequency sweeping method; step 3, correlating received data with the PN sequence A after compensation carrier is subjected to large frequency offset, so as to estimate a serial number of a frame; generating a PN sequence B of a matched phase matched with the frame header mode, and then correlating the PN sequence B with the received data so as to obtain a frame header position fine estimation value; and step 4, carrying out self-correlation on the frame header position according to the frame header position fine estimation value so as to obtain a carrier frequency offset fine estimation value, and summarizing a carrier frequency large offset estimation value and the carrier frequency offset fine estimation value so as to obtain a final carrier frequency offset estimation value. In the invention, the time-frequency synchronization joint estimation method based on the multi-carrier receiver of the DTMB system is used, thereby facilitating the realization of share of operation data and parameters and reducing the arithmetic labor.
Owner:FUZHOU UNIV

Low-orbit/middle-orbit double-layer satellite optical network structure system and design calculation method

InactiveCN101604996ATopologically stableSimplified routingElectromagnetic network arrangementsZero phaseNetwork structure
The invention discloses a low-orbit/middle-orbit double-layer satellite optical network structure system. Global coverage low-orbit satellite constellation designed on the basis of a coverage zone method and middle-orbit satellite constellation form a double-layer satellite optical network structure system. The system is connected with at least 76 satellites, wherein, a low-orbit satellite layer is provided with at least 7 orbits, and each orbit is connected with at least 10 satellites; a middle-orbit satellite layer is composed of an outer orbit and an inner orbit, wherein, the outer orbit is respectively connected with the satellites, and the inner orbit is respectively connected with the satellites. The calculation method is as follows: calculating the radius theta of a single satellite covering circle; calculating the halfangle psi of the covering zone; calculating delta B; calculating alpha'; calculating sin alpha; and calculating the distribution of P orbits on the equator. The structure is stable topological structure, the changes of inter-satellite links pitch angle and azimuth angle are smaller than the changes of the inter-satellite links pitch angle and the azimuth angle of the non-zero phase constellation, satellite switch is reduced, satellite-carried resources are saved, and management of the low-orbit satellite layer is effectively strengthened; the middle-orbit satellite constellation is least affected by space radiation, and the system life cycle is lengthened.
Owner:AIR FORCE UNIV PLA

Ion accelerator injection device and using method

The invention relates to an ion accelerator injection device, and belongs to the technical field of nuclear energy. The ion accelerator injection device is characterized in that the ion accelerator injection device comprises an ion beam current ECR ion source, a first solenoid, a second solenoid, an RFQ linear accelerator and a mixed type ion accelerating device, wherein the ion beam current ECR ion source is used for generating high intensity, and the first solenoid and the second solenoid are connected with the RFQ linear accelerator and the mixed type ion accelerating device through vacuum pipelines. The RFQ linear accelerator and the mixed type ion accelerating device are connected through a flange. The ion accelerator injection device has the advantages that in the accelerating process of high intensity ion beam currents, the quality of the beam currents is made to be better due to the fact that the structure is more compact; the accelerating function and the transverse and longitudinal focusing function are combined in the same high-frequency structure by using the accelerating function of a mixed type DTL, cavity shunt impedance is high, and high-frequency power dissipation is lowered greatly; acceleration is carried out by using a zero phase, acceleration efficiency is higher, the length of a cavity can be reduced effectively, and effective accelerating gradients can be improved; an additional transmission matching section is not needed between an RFQ and the mixed type DTL, manufacturing cost can be lowered, and the length of the device can be shortened. The ion accelerator injection device is mainly applied to acceleration of high intensity low energy ion beam currents, and can be applied to injection devices of high-current accelerators, industrial accelerators and other application type accelerating devices.
Owner:INST OF MODERN PHYSICS CHINESE ACADEMY OF SCI
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