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Method of adjustment of optical axis of viewfinder and electrical axis of aerial |
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IPC classes for russian patent Method of adjustment of optical axis of viewfinder and electrical axis of aerial (RU 2252427):
Device for changing area of reflecting surface / 2244940
Cavity of radio-transparent envelope which has to be model of tested object is partially filled with electrically conducting liquid. Level of liquid is controlled by piston pump and measured by level meter. Radio-transparent cavity has a shape of circular cylinder with preset sizes which shape allows reproduce "selection" of standard reflectors in form of circular cylinders at smooth change in level of electrically conducting liquid. Values of dissipation effective areas of the cylinders can be calculated with high precision. Radio-transparent envelope can have shape of cylindrical pipe.
Device for measuring effective scattering cross-section of object / 2244939
Device for measuring effective scattering cross-section of radio-location objects has receiving-transmitting unit, registrar, stand mounted for rotation and provided with fixing unit which is used for mounting test object oriented in such a manner that normal to flat front of electromagnet wave radiated by receiving-transmitting unit belongs to preset plane of rotation of object. Precision inspection of measurement of angular diagram of effective scattering cross-section of objects provided due to the fact that radio-transparent envelope is rigidly fixed on the surface of object in parallel with preset plane of rotation of object. Radio-transparent envelope is made in form of thin straight cylinder of preset size. Cavity of envelope is partially filled with e4lectrically conducting liquid. Measured maximal level of effective scattering cross-section of main lobe of radio-transparent cylinder allows to find angle of inclination of plane of rotation of object.
Device for measuring effective scattering cross-section of object / 2244939
Device for measuring effective scattering cross-section of radio-location objects has receiving-transmitting unit, registrar, stand mounted for rotation and provided with fixing unit which is used for mounting test object oriented in such a manner that normal to flat front of electromagnet wave radiated by receiving-transmitting unit belongs to preset plane of rotation of object. Precision inspection of measurement of angular diagram of effective scattering cross-section of objects provided due to the fact that radio-transparent envelope is rigidly fixed on the surface of object in parallel with preset plane of rotation of object. Radio-transparent envelope is made in form of thin straight cylinder of preset size. Cavity of envelope is partially filled with e4lectrically conducting liquid. Measured maximal level of effective scattering cross-section of main lobe of radio-transparent cylinder allows to find angle of inclination of plane of rotation of object.
Device for changing area of reflecting surface / 2244940
Cavity of radio-transparent envelope which has to be model of tested object is partially filled with electrically conducting liquid. Level of liquid is controlled by piston pump and measured by level meter. Radio-transparent cavity has a shape of circular cylinder with preset sizes which shape allows reproduce "selection" of standard reflectors in form of circular cylinders at smooth change in level of electrically conducting liquid. Values of dissipation effective areas of the cylinders can be calculated with high precision. Radio-transparent envelope can have shape of cylindrical pipe.
Method of adjustment of optical axis of viewfinder and electrical axis of aerial / 2252427
Viewfinder is disposed at specific distance from mechanical axis of aerial. Viewfinder is tightly connected with antenna aperture plane. Optical axis of viewfinder is directed in parallel to mechanical axis of aerial. Then electrical axis of aerial is guided to phase center of ancillary aerial which is disposed together with geodetic mark onto post. Optical axis of viewfinder is guided onto geodetic mark. Geodetic mark is tied to angular position detectors and stays apart from phase center of ancillary aerial for distance being equal to shift of viewfinder from mechanical axis of aerial to the plane of normal optical axis of viewfinder. Optical axis of viewfinder is guided onto center of aperture of ancillary aerial. Difference in coordinates is determined by angle of location of initial and final position of viewfinder optical axis. Sword is turned around axis being perpendicular to plane of sword and crossing center of ancillary aerial aperture by angle determined by the relation given in the description of the invention. Electrical axis of aerial is guided onto phase center of ancillary aerial and optical axis of viewfinder is guided onto geodetic mark.
Method of inspecting parameters of aerial systems / 2254585
Method can be used for tuning and inspecting code on-board detectors of transportation vehicle automatic identification telemetric system. Section of reference aerial is calibrated in echo-free reference chamber inside which non-modulated oscillations are excited by connecting load in form of light-emitting diode cell to reference aerial. Fiber-optic section provided with light-receiving device and pre-calibrated indicator are also connected to reference aerial. Tested aerial is placed into the field induced by oscillator and measuring aerial inside working echo-free medium. The field is pre-calibrated by attenuator corresponding to readings of indicator of the reference aerial placed in the field before placing tested aerial inside the field.
Method for adjustment of radiolocation station antenna / 2262117
Method includes using auxiliary antenna and geodesic mark, linked with indicators of angular position of target antenna, viewfinder is positioned near opening of subject antenna, rigidly linked to opening plane of subject antenna. Flat metallic screen is inserted, to which emission from auxiliary antenna is directed, auxiliary antenna and geodesic mark as light source are positioned behind subject antenna at remote zone distance. Electric axis of subject antenna is directed using its rotation gear according to one of minimum methods to phase center of auxiliary antenna, screen is mounted so, that beams, falling o it from auxiliary antenna and geodesic mark, were reflected respectively to whole plane of opening of target antenna and inlet eye of viewfinder. Angular deflection of optical axis of viewfinder from direction to center of image of geodesic mark on screen determines adjustment of target antenna.
Method of measurement of complex excitement amplitude of channels of phased array / 2267795
Method can be used for measurement of directional pattern of phased arrays and detection of damaged channels of phase array when using standard equipment of radar installations which have phased arrays as a part of equipment. Super-high frequency control signal is generated and irradiated by motionless probe at the direction of phased array. Control signal is received by phased array at alternate modulation of signal phase of each channel of phased array and signal is subject to coherent conversion to video frequency followed by selection of quadrature-phase component. Channel is switched to any phase state only once and at any phase state of the channel the analog signal is transformed into digital one K times (value of K varies from 100 to 10000 and higher depending on number of channels). Digital indications are rearranged in such a way that phase of signal of commutated channel in adjacent readings would differ for discrete value of switching of channel's phase. Signal spectrum is calculated. All the spectral components are reduced excluding components of useful signal which number equals to number of phase states of channel. Spectral component corresponding to zero frequency is reduced to zero. Fourier anti-transform is calculated. The sequence calculated has to represent complex excitement amplitudes for any phase state of channel.
Device for measurement of amplitude-phase field distribution in receiving aerial aperture / 2275646
Device for measurement amplitude-phase field distribution in receiving aerial aperture has super-high frequency generator. Output of the generator is connected with measuring probe and with first input of amplitude-phase meter. Output of the latter is connected with first input of data collection and control device. First input of the latter is connected with first input of first computational unit intended for memorizing measured relations of signal amplitudes and phases and for computing amplitude-phase distribution. Device for measurement amplitude-phase distribution has turn unit being mechanically connected with tested aerial which has output connected with second input of amplitude-phase meter. Data collection and control unit serves for forming and outputting control commands to turn unit and for controlling measurement device in total. Device also has second computational unit intended for computing coordinates of points of measurement of tested aerial's transmission factor vector correspondingly to optimal spatial structure of measurement and memory unit intended for storing information on spatial configuration of the aerial. Output of second computational unit is connected with second input of information collection and control unit and with second input of first computational unit. Output of memory unit is connected with input of second computational unit and with third input of first computational unit. Memory unit is mounted onto tested aerial.
Stand for measuring parameters of reflector / 2276793
Echo-less chamber, including reflector, receiving technological antenna and system of transmitting cone-shaped irradiators, is provided with system of pulling and adjusting ropes made of resilient radio-transparent material. On aforementioned ropes, receiving technological antenna is held with possible movement by adjusting length of ropes, optical axis of antenna is directed perpendicularly to phase front of electromagnetic wave reflected by reflector. System of transmitting cone-shaped irradiators is connected to adjusting rope and held on a console, which is made of durable rigid radio-transparent material and held on the wall of echo-less chamber.
Radar measurement compensation-type installation with continuous radiation / 2278391
Installation can be used for measurement of radar characteristics (amplitude and phase diagrams) off dissipation for objects with different shapes. Radar compensation-type measurement installation with continuous radiation has diffuser, bed of diffuser, rotary unit, angle meter, reference signal generator, first attenuator, oriented de-coupler, matching transformer, second attenuator, double wave-guide T-bridge, load, transmitting aerial and receiving aerial. Unit for measuring difference in phases and level relation is introduced into installation additionally as well as control and processing unit, rotary unit control device and amplifier. Time of measurement is reduced due to complete automation of measurement of reverse dissipation process of real objects is provided.
Method of measurement of antenna directivity diagram / 2279100
Method can be used for inspection of directivity diagrams of antenna systems of different radio systems. Method is based upon measurement of signal amplitude of point radio signal source, disposed in far area of antenna, and angular coordinates of the source. Several navigation satellites of global positioning systems GPS are used. Data on amplitude of radio signals of navigation satellites, their angular coordinates and preudorange to navigation satellite are presented in Internet in form of files in RINEX formats. Rows of values of radio signal amplitudes are formed by means of processing of RINEX files for any navigation satellite depending on its angular coordinates. Rows are selected of set of rows achieved for angles of location of navigation satellite being bigger than 10° which are controlled for factors being proportional to pseudorange till getting corresponding to navigation satellites. Rows of controlled values of amplitude for all the navigation satellites are coherently supposed to adding and averaging.
Method of adjustment of optical axis of viewfinder and electrical axis of aerial / 2252427
Viewfinder is disposed at specific distance from mechanical axis of aerial. Viewfinder is tightly connected with antenna aperture plane. Optical axis of viewfinder is directed in parallel to mechanical axis of aerial. Then electrical axis of aerial is guided to phase center of ancillary aerial which is disposed together with geodetic mark onto post. Optical axis of viewfinder is guided onto geodetic mark. Geodetic mark is tied to angular position detectors and stays apart from phase center of ancillary aerial for distance being equal to shift of viewfinder from mechanical axis of aerial to the plane of normal optical axis of viewfinder. Optical axis of viewfinder is guided onto center of aperture of ancillary aerial. Difference in coordinates is determined by angle of location of initial and final position of viewfinder optical axis. Sword is turned around axis being perpendicular to plane of sword and crossing center of ancillary aerial aperture by angle determined by the relation given in the description of the invention. Electrical axis of aerial is guided onto phase center of ancillary aerial and optical axis of viewfinder is guided onto geodetic mark.
Target fluctuating signal generator / 2253129
The device having a control panel, storage unit, synchrosignal generator, first, second and third on-line memories, unit for formation of target relative coordinates, unit for formation of the maximum target signal intensity, first, second, third and fourth synchronizers, unit for formation of the current intensity of the target signal, digital-to-analog converter, noise generator, adder uses also a correlator, first and second detectors, first and second multiplier units, first and second random number generators, which provides for formation of amicably fluctuating and quickly fluctuating bursts of pulses reflected from the radar targets, internal noise of the receiver and synchronizing signals at the output of the radar receiver in the rate of radar functioning and with due account made for motion of the ship-carrier.
Generator of reflected radar signals from disturbed sea surface / 2253130
The device has a control panel, memory unit, preliminary recording control unit, unit for formation of carrier relative coordinates, readout and synchronizing unit, on-line memory unit, unit for formation of video signal, unit for formation of carrier polar coordinates, noise formation unit.
Mode of controlling working capacity of airborne receiver indicator of satellite radio navigational system / 2254591
The mode is that the altitude HRA of the flight of a flying vehicle is measured with the help of installed on it a radio altimeter (RA), the altitude hr of an area above which a flying vehicle flies at the moment of the altitude measuring using for this purpose data about planned coordinates from the output of the receiver indicator of the satellite radio navigational system and digital map of an area, an absolute altitude Ha= HRA +hr, is calculated and compared with the altitude HRI, taking from the output of the receiver indicator and a signal of its working capacity is formed if |Ha- HRI| is smaller than the installed threshold Th.
Radio-signal dynamic memory device having series binary fiber- optic system / 2255426
In order to enhance identity of copy generation while retaining ability of controlling input radio signal replication process, proposed device is provided with newly introduced (N -1) fiber-optic four-terminal networks, each of them incorporating Y-type internal adding and separating fiber-optic directional couplers.
Radio engineering training device / 2260193
Device has radio-location station, first high-frequency generator, modulator, first counter, scanning generator, second counter, heterodyne, first mixer, first intermediate frequency amplifier, first amplitude detector, video-amplifier, third counter, cathode-ray tube, second, third and fourth high-frequency generators, first and second adders, switches, phase-rotators and on 90°, second mixer, second intermediate frequency amplifier, multiplier, narrow-band filter, second amplitude detector, key and frequency converter.
Method for adjustment of radiolocation station antenna / 2262117
Method includes using auxiliary antenna and geodesic mark, linked with indicators of angular position of target antenna, viewfinder is positioned near opening of subject antenna, rigidly linked to opening plane of subject antenna. Flat metallic screen is inserted, to which emission from auxiliary antenna is directed, auxiliary antenna and geodesic mark as light source are positioned behind subject antenna at remote zone distance. Electric axis of subject antenna is directed using its rotation gear according to one of minimum methods to phase center of auxiliary antenna, screen is mounted so, that beams, falling o it from auxiliary antenna and geodesic mark, were reflected respectively to whole plane of opening of target antenna and inlet eye of viewfinder. Angular deflection of optical axis of viewfinder from direction to center of image of geodesic mark on screen determines adjustment of target antenna.
Radar target simulator / 2267798
The radar target simulator has a super high frequency module consisting of successively connected arrangements: an automatic regulator of power, an impulse modulator, an amplitude modulator, a switch of the power level and a digital attenuator, a communication line, a horn antenna, a group of keys, the first semiconductor storage, an interface of a multiplex bus, a synthesizer of Doppler frequencies, a second semiconductor storage and a multiplying digital-analogue converter. The increasing of the accuracy of the installation of the output power is provided due to possibility of its correction by way of changing the intensity of the amplitude modulation of the super high signal for each meaning of the value of fading.
Emulation device of an active response radar connected with a surveillance radar / 2268477
It is also used for instruction and training of the operators of the surveillance facilities connected with an active response radars in the conditions of the presence of a great number of targets moving on complex trajectories. The essence of the invention is in that the arrangement holds an oscillator of the signals of the targets including the targets carrying responders. In it there is a control panel of the active response radar, a selector of characteristics of response signals, a synchronizer of response signals, an operating response signals storage device, a decoder of the characteristics of response signals, a counter of tact impulses, a former of identification markers and an adder unit with their connections that provides emulation of the operation of the active response radar connected with the surveillance radar at changing their modes of operations in the process of obtaining radar information about common and individual characteristics of the target carrying a responder in the zone of operations of the mentioned radar facilities with the purpose of verification of their terminal facilities of the secondary processing of radar information, instruction and training of the operators of the surveillance radar.
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FIELD: radiolocation. SUBSTANCE: viewfinder is disposed at specific distance from mechanical axis of aerial. Viewfinder is tightly connected with antenna aperture plane. Optical axis of viewfinder is directed in parallel to mechanical axis of aerial. Then electrical axis of aerial is guided to phase center of ancillary aerial which is disposed together with geodetic mark onto post. Optical axis of viewfinder is guided onto geodetic mark. Geodetic mark is tied to angular position detectors and stays apart from phase center of ancillary aerial for distance being equal to shift of viewfinder from mechanical axis of aerial to the plane of normal optical axis of viewfinder. Optical axis of viewfinder is guided onto center of aperture of ancillary aerial. Difference in coordinates is determined by angle of location of initial and final position of viewfinder optical axis. Sword is turned around axis being perpendicular to plane of sword and crossing center of ancillary aerial aperture by angle determined by the relation given in the description of the invention. Electrical axis of aerial is guided onto phase center of ancillary aerial and optical axis of viewfinder is guided onto geodetic mark. EFFECT: improved precision of adjustment. 2 dwg
Now the present invention relates to the field of radar and can be used when aligning the antenna of the radar stations. Under the alignment of the antenna refers to the setting of relative position in space of the reference axis of the antenna associated with the sensors of its angular position, and the electrical axis of the antenna. The location of the reference axis in the binding process sensors on geodetic marks on the ground is carried out using optical instruments. For axisymmetric mirror antenna alignment checks for the axis deviation of the antenna from the optical axis of the reticle installed parallel to the geometric axis of the antenna. There is a method of determining the angular deviation of the axis of the reticle from the electrical axis of the antenna [1], which is as follows: near the aperture of the antenna 1 at a certain distance from the axis of the antenna set and rigidly connected with the plane of the aperture of the reticle 2 with coordinates a and b along the axes X and Y (see figure 1). On the tower 3 located at a certain distance from the antenna, install the shield 4, which is placed geodetic mark 6 and the auxiliary antenna 5 as a radiator. Geodetic mark 6 is removed from the phase center auxiliary antenna 6 at distances a and b along the axes X’ and Y’equal to the displacement of the reticle 2 from the axis of the antenna 1 in the plane, n is malnoy line of sight. For geodetic Marche 6 cable sensors angular position of the antenna 1. The electrical axis of the antenna 1 by the methods of minimum of [2] are sent to the phase center of the auxiliary antenna 5. If the optical axis of the sight is not parallel to the electrical axis of the antenna, the cross hair will not coincide with the geodetic mark. On the angular deviation of the optical axis of the reticle from the direction to the geodetic mark determine the angle between the optical axis of the reticle and the electrical axis of the antenna. This solution has a major drawback. To the position of the geodetic marks exactly correspond to the position of the reticle on the distance from the phase center of the auxiliary antenna, the coordinate axes X and X’ or Y and Y’ must be parallel. Otherwise, an error occurs when determining the angular deviation of the optical axis of the reticle from the electrical axis of the antenna and the greater the angle between the axes X and X’, the greater will be the error. In practice rig (Y axis’) and azimuthal axis of antenna rotation (Y axis) is some angle that causes the error when determining the angular deviation of the optical axis of the reticle from the electrical axis of the antenna. The task of the invention is to improve the accuracy of alignment of the optical axis of the reticle and the electrical axis of the antenna. The solution of this problem is achieved by the fact that the act is both the alignment of the optical axis of the reticle with the electrical axis of the antenna, which consists in placing at a certain distance from the mechanical axis of the antenna of the Vizir, rigidly connected to the plane of the aperture, the optical axis is set parallel to the mechanical axis of the antenna, pointing methods minimum electrical axis of the antenna phase center auxiliary antenna located together with geodetic mark on the tower, and the alignment of the optic axis of the reticle mark on the geodesic and geodesic brand is bound to the sensors of the angular position of the antenna and removed from the phase center auxiliary antenna by a distance equal to the offset of the reticle from the mechanical axis of the antenna in the plane normal to the optical axis of the viewfinder, advanced optical axis of the camera is directed to the center of the aperture of the auxiliary antenna, determine the difference between the coordinates in elevation of the initial and end positions of the optical axis of the reticle and the shield rotates around an axis perpendicular to its plane and passing through the center of aperture of the auxiliary antenna on the corner where α1that α2values of the sensor of angular position of the antenna in elevation, respectively, when the target channel was aimed at surveying the brand and on the phase center auxiliary antenna; L is the distance between the auxiliary antenna and the Vizir And the geodesic distance between the brand and the center of the aperture of the auxiliary antenna. Then bring the electrical axis of the antenna phase center auxiliary antenna and the optical axis of the reticle on geodetic mark. The proposed method is illustrated by figure 2, where 1 - ushiroyama antenna; 2 - Vizir; 3 - tower; 4 - shield 5 - auxiliary antenna; 6 - geodetic mark. The method of aligning the optical axis of the reticle and the electrical axis of the antenna is as follows: near the aperture esteruelas antenna 1 is installed and rigidly connected with the plane of the aperture of the reticle 2 (see figure 2) with coordinates And the X-axis and 0 on the axis Y. the Y Axis parallel to the azimuth axis of rotation of the antenna 1, and the origin of coordinates coincides with the mechanical axis of the antenna 1. At a certain distance from esteruelas antenna 1 is installed tower 3, and on it place the shield 4. On the shield have 4 auxiliary antenna 5 as emitter and geodetic mark 6. In the coordinate system X’, Y’ geodetic mark 6 has coordinates along the axes X’ and 0 on the Y-axis’. Axis X’, Y’ respectively parallel to the axes X, Y. the origin of coordinates X’, Y’ coincides with the phase center auxiliary antenna 5. For geodetic Marche 6 cable sensors angular position of the antenna 1. Using the rotator antenna 1 electric the forge axis of the antenna 1 by the usual methods of minimum of [2] suggest the phase center auxiliary antenna 5. Then the optical axis of the camera is directed to the center of the aperture of the auxiliary antenna 5 and determine the difference between the coordinates in elevation of the original α1and the final α2the position of the optical axis of the reticle. This operation is carried out to determine the angle between the axes X and X’. If the axes are parallel, that α1=α2. If the angle between the axes X and X’ shield rotates around an axis perpendicular to its plane and passing through the center of aperture of the auxiliary antenna on the corner γ. After the performed operation axis Y’ and become parallel. Then bring the electrical axis of the antenna phase center auxiliary antenna and the optical axis of the reticle mark on the geodesic. As a result of operations with great precision set the optical axis of the camera parallel to the electrical axis of the antenna. Sources of information 1 Lntegral, Lai, Vietoris and other Methods of measuring the characteristics of microwave antennas. Edited Namzatovna. - M, Radio and communications, 1985, - 114 C. 2 Umizaru, Whackaloons, Ukito and other Radio system. - M, Owls. radio, 1986, - 40-44 C. The method of aligning the optical axis of the reticle and the electrical axis of the antenna, which consists in placing at a certain distance from the mechanical axis of the antenna of the Vizir, rigidly connected to the plane of the aperture of the antenna, the optical axis is set parallel to the mechanical axis of the antenna, pointing methods minimum electrical axis of the antenna phase center auxiliary antenna located together with geodetic mark on the shield installed on the tower, and the alignment of the optic axis of the reticle mark on the geodesic, while the geodetic mark attached to the sensors of the angular position of the antenna and removed from the center of the aperture of the auxiliary antenna by a distance equal to the offset of the reticle from the mechanical axis of the antenna in the plane normal to the optical axis of the reticle, wherein induce optical axis of the reticle on the center of the aperture of the auxiliary antenna, determine the difference between the coordinates in elevation of the initial and final provisions the optical axis of the viewfinder and turn the shield around an axis perpendicular to the plane of the shield and passing through the center of aperture of the auxiliary antenna on the corner where α1that α2values of the sensor of angular position of the antenna in elevation, respectively, when the optical axis of the reticle is aimed at surveying the brand and the center of the aperture of the auxiliary antenna; L is the distance between the auxiliary antenna and the Vizir; And the geodesic distance between the brand and the center of the aperture vspomogatelnaya, then bring the electrical axis of the antenna phase center auxiliary antenna and the optical axis of the reticle on geodetic mark.
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