Ranging method and device to determine coordinates of radiation source. RU patent 2506605.
 Additional data used to determine location of device / 2505833Device can determine whether to provide in a packet information used to determine location, and if it is determined that location information can be provided in the packet, the header information in the packet can be configured to indicate that the packet contains location information, and to indicate the type of that information. Said information can then be included in the transmitted packet. If the packet is an advertising packet, the packet can be transmitted over an advertising channel. The device searching for signals can then receive the packet and, based on the header information in the packet, determine whether the packet contains location information. If it is determined that the packet contains location information, location in the device searching for signals can be configured based in the header information, and location can be performed in the device searching for signals based on the location information contained in the packet. |
 Method of determining coordinates of aerial objects in passive bistatic radar / 2504797Invention is intended to determine coordinates of aerial objects from signals of a radar identification system without receiving signals of interrogation radar, the location of which is known. The novelty is detection, based on the time structure interrogation radar radiation of the radar identification system, of signal packets of an onboard transponder with an unknown location, the i-th of which is selected as a "reference", extrapolation of the time of receiving signals thereof, selecting signal packets of the j-th onboard transponder with a known location, calculating the delay time of propagation of signals "interrogation radar - j-th onboard transponder - reception unit" and "interrogation radar - reception unit", followed by transitioning to extrapolation of the time of receiving interrogation radar signals, determining coordinates of the aerial object through the values of parameters of two position lines - elliptical and the line of the constant bearing from the position of the interrogation radar. |
 System of monitoring products/operation with high reliability / 2502081Monitoring system includes a monitoring device and a verification server. The monitoring device is connected to a first receiving device for satellite positioning, which is configured to receive signals from a satellite positioning system, process the received signals to obtain observed satellite positioning parameters and calculate a position based on the observed satellite positioning parameters. The monitoring device selects an observed satellite positioning parameter based on which a position is calculated using the first receiving device for satellite positioning, and obtain from the receiving device for satellite positioning the selected observed satellite positioning parameter. The verification server verifies position consistency based on the position and based on the observed satellite positioning parameter. The verification server is further configured to generate an authentication code based on the position consistency verification result and based on positioning data. |
 Device for joint treatment of course measurement results in mobile device by gnss-compass and stabiliser gyrocompass / 2488843Threshold device is introduced to reduce error components specified by accidental release of course measurement results by a GNSS compass, and also a multichannel discrete filter providing, within the proposed circuit solution, for reduction of dynamic error components specified by unpredictable manoeuvres of a mobile device by speed and direction. |
 Method of automatic control of warehousing platform trucks and device for its implementation / 2470316Invention relates to the field of instrument making and may be used in organisation of safe and convenient method of warehousing in automated systems of cargo processing and storage (AS/RS). To achieve the result, a unit is introduced from N discrete sensors of relay type arranged in N reference points, and an organ of information signals processing, the input of which is connected to an output of the communication channel, and also a unit of summing scaled currents with a scaling ratio by each input that are proportional to the number of this input, besides, the i input of the scaled currents summing unit is connected to the output of the i sensor, and the output of the scaled currents summing unit is connected to the input of the communication channel, an agent of information processing, comprises a unit of current conversion into voltage, a subtractor, an analogue to digital converter, a calculator, a memory unit, a digital to analogue converter, a threshold element, an RS-trigger, a gate multivibrator and two elements of signal delay. |
 Method for locating satellite communication earth station / 2442996FIELD: satellite control systems. SUBSTANCE: satellite control system antenna is pointed on the satellite retranslating the signal of this earth station. Measuring receiver is connected to the antenna-feeder tract of the SCS station and is used to measure mean square value of retranslated signal power from simultaneously operating through retranslating satellite reference earth stations with known earth coordinates and target ES. The measurements are performed in discrete moments of time on fixed frequency of retranslated signals of ES on the observation interval TH. The results of measurements are recorded in text files and are presented in form of curves (fig.1) where on the horizontal axis there are counting numbers n=0,1,2….,N - numbering of counting with spacing Δt with Δt=const, Δt -interval between counting, and on the vertical axis there are values of counting equal to signal levels yq(n), q=1,2,…, q- numbering of earth stations. Using visual analysis of the dependences long-term cyclic repetition of signal level fall with short-living high frequency components. Fall of signal level is associated with its weakening when the ES- retranslating satellite is passing through the areas of volumetrically distributed hydrometeors (VDH). With such repetitions on the observation interval TH the detailed information is determined on dynamic properties of signals - parameters of reviewed repetitions (beginning, duration, ending). In order to get it the procedure of processing of discrete sequences of signal counting yq(n) is performed using the software means of discrete wavelength transformer on the base of basic Dobeshi wavelength of the 1st order on PC in MathLab program. Discrete sequences of signal counting yq(n) are decomposed into refining wavelength-coefficients 1d,n where d=1,2,…, D - numbering of decomposition level of different scope of signal dynamic with D≤log2N. Refining wavelength-coefficients 1d,n are presented in form of curves (fig.2) where on the horizontal axis are number of counting n, and on the vertical counting - values of refining wavelength-rations 1d,n that show on selected decomposition level d in different scope dynamic properties of the signal - parameters of cyclic repetition of signal level falls (beginning, duration, amount). Using visual analysis of the curves the similarity of such parameters is detected between target ES and at least one reference ES. Based on the geometric presentation of the method (fig.3) showing local homogenous area of VDH, central prospective projection of such area on the Earth surface and routes ES-retranslating satellite, it is thought that the similarity is caused by routes ES-retranslating satellite passing through the same VDH area with limited occupying space and condition of passing of different routes ES-retranslating satellite through VDH area with such characteristics is territorial proximity of ES. The area of most probable location of target ES is determined by referencing the earth coordinates of reference ES that is similar to target ES in dynamics of retranslated signals levels. EFFECT: simplification and decreased realization cost of the method achieved due to locating earth station (ES) in the abovementioned way. 1 dwg, 3 dwg |
| Method for visual navigation on sea / 2437115 Energy is stored in an accumulator and the flash diagram of a light source is programmed. The main light source is switched on at night. Programmed light flashes are generated. Radiation of the light source is formed by an optical lens of different colour in separate sectors, and if the main light source runs out of power, the accumulator of the backup light source is switched on. The flash diagrams of several light sources are synchronised. The main light source is powered from the main accumulator, and the backup accumulator is charged from the main accumulator. The light source used is series-connected light-emitting diodes. A lens which forms light flux is placed on each light-emitting diode. The colour of the light is determined by the light-emitting diode. A sector of different colour is formed from some of the light-emitting diodes. Navigation is allowed in white-coloured sectors. |
 Method of configuring integral destruction zone of fire units / 2430384Proposed method is intended for estimating fire system efficiency and determining parameters of combat control in computer-based ACS of force units. In compliance with proposed method, parameters of destruction zone of local fire units are used to define parameters of spatial integral destruction zone of fire units group to simplify determining spatial and time characteristics of target with respect to fire unit zone and to increase efficiency of target selection at the level of fire detachments. Obtained integral zone allows defining target trajectory in said zone, time of target crossing said zone, time of target entry into and exit from said zone, selecting target in due time, that is, to allow destructing target at destruction zone boundary with due allowance for limited target height and parameter processing possibilities. |
 Target triangulation method / 2423720Target triangulation method employs a method of determining three spatial coordinates of a target based on information from two-dimensional direction finders which independently measure the azimuth and position angle of the object. Said method involves determination of the approach point of bearings in space. The determined point lies at minimum distance from two bearings. The bearing of the target is given by the stand point of the bearing source and the direction to the target from the stand point. The stand point is defined by coordinates (x, y, h) and the direction to the target is given by the azimuth and position angle. Parameters are given in the left-side rectangular coordinate system. The method enables to determine additional data of the spatial position of bearings in the vicinity of the approach point. |
 Method of defining angular orientation of object / 2422844Proposed method comprises obtaining data on coordinates of moving object from onboard inertial navigation system, receiving signals from satellite radio navigation system by three navigation receiver antennas A0, A1, A2 fixed on moving object and not located on one straight line, data processing to define angular orientation parameters. Note here that data processing comprises correcting errors in angular orientation parameters received from inertial navigation system using signals from one available satellite and their phase difference received by spaced apart antennas A0 and A1 to define angle β1 between antenna datum d1 and direction to satellite. Data received from onboard inertial navigation system about coordinates and orientation parameters and that from satellite navigation system on satellite coordinates are used to define angle β1* between antenna datum d1 and direction to satellite by phase difference of signals received from satellite by spaced apart antennas A0 and A2. Angle β2 between antenna datum d2 and direction to satellite is defined. Data received from onboard inertial navigation system about coordinates and orientation parameters and that from satellite navigation system on satellite coordinates are used to define angle β2* between antenna datum d2 and direction to satellite is defined. In case magnitudes β1 and β1*, β2 and β2* differ by quantity exceeding preset one, error is corrected in angular orientation parameters received from onboard inertial navigation system. |
 Method for receiving and actualization of digital cartographic material and device for realization of said method / 2244260Method includes forming matrix for transforming image or objects coordinates distortion matrix on certain digital plans and symbolic circuits relatively to true geographic coordinates received for tracked objects via navigation devices of users, by combining plans or symbolic circuits with precise terrain chart. Distortion matrix is included in contour of displaying objects on plans and circuits, on basis of true geographic coordinates of tracked objects, sent in by users. A layer of plan or circuit of terrain transformed according to matrix is formed, on which tracked objects are marked by certain graphic symbols. Data, received on circuit, for example, route and movement speed of each tracked object, is relayed to certain users with visualization of symbolic circuit on indication device of each user. Device for realization of method has digital terrain chart, received information processing device, information indication device, n components of subscribers complex. Each component has device for determining coordinates on terrain connected by its input to output of controlling device, directly or through encoder/decoder. Outputs of control device are connected to inputs of information indication device and to device for connecting to radio channel. Device for connecting each subscriber component to radio channel is connected by its input to output of control device and is connected to group device for connecting to radio channel belonging to base portion of device for receiving digital cartographic material. Another input and output of group device for connecting to radio channel are connected directly to output and input of coordinates transforming and controlling device or respectively to output and input of second encoder/decoder, connected by other its input and output respectively to output and input of device for coordinates transformation and control. Another input of coordinates transformation and control device is connected to output of distortion matrix storage device. Next input and output of coordinates transformation and control device are connected respectively to output and input of block, containing digital terrain charts and to output and input of block, containing symbolic circuits or plans of same terrain. |
 Method for increasing kinematic mode range of real-time determination of relative coordinates of object / 2247406Method comprises steps of additionally transmitting from reference point parameters that allow to calculate coordinates of navigation spatial apparatuses at higher accuracy. Relation of error value of range measurement and error values of coordinates of navigation spatial apparatus is determined according to expression: , where b - distance between reference and determined points; R - distance between reference point and navigation spatial apparatus; L - vector value of coordinate errors of navigation spatial apparatus. |
 Method of determining angular orientation of object / 2248004Method comprises receiving signals by spaced signal receivers which are not aligned. The signal receivers are made of at least three GPS-receivers. |
 Method of precision positioning and monitoring of mobile objects / 2248005"m" monitoring and correcting stations are formed around TV center, where "m" is any integer of navigation spacecraft forming local differential corrections which are transmitted to TV center via radio channel and then to mobile object through TV center transmitter without impairing present broadcasting; mobile object determines its coordinates by signals of navigation spacecraft with local differential corrections taken into account; coordinates thus determined are transmitted to TV center via radio channel and then they are transmitted to traffic control station; traffic control signals formed at traffic control station are transmitted together with coordinates of mobile object to nearest dispatching station by satellite communication channels where target designation signals are formed and are transmitted to mobile object. |
 Mode and arrangement of dual-range synthesizer of a lettered frequency of the satellite navigational system glonass / 2251121For this purpose two oscillators of a lettered frequency and of a fixed frequency are used. Mode includes successive fulfillment of the following operations - generation of a stabilized lettered frequency, its multiplication with an oscillator's fixed frequency and filtration of lateral multipliers with means of filters of L1 and L2 ranges and corresponding option of a fixed and a lettered frequencies. |
 Systems and methods for solving ambiguity on basis of effective pseudo-distance of global positioning system / 2253127Mobile terminal has satellite phone and global positioning system receiver, using information concerning position of trace of antenna beam of communications satellite, within reach of which mobile terminal is positioned. By using said information, current invention provides for solving ambiguity, in form of one millisecond, which occurs as a result of length of code repeat, when relative phrase of code can be determined, while absolute phrase of code can not be determined. Test positions are selected for covering area of trace of antenna beam with spaces between test positions, considering indeterminacy, in form of one millisecond. Measured values of pseudo-distance are produced for each test position and used to determine position. Best determined result is selected, for example, on basis of check of self-consistency. |
 Method for determination of object relative coordinates with survey to arbitrary point of space and system for its realization / 2253128Correlation (reduction) of the parameters (velocities and ranges) to the coordinates of the space arbitrary point (virtual point) is accomplished at a reference station. |
 Method of and device for measuring geometry of track / 2256575Geometry of track is measured by using high-accuracy measuring circuit with two mechanically coupled test trucks forming transport and mechanically coupled test trucks forming transport and mechanical part of measuring system and including covered distance meter and truck tilting level sensors relative to horizon and at least one radiating mark (optical radiation source) rigidly installed on first test truck in direction of movement and providing pressing of flange of wheel to inner head of base rail, and optical electronic receiving-and-analyzing system rigidly secured on second truck. Second truck is double axle, with flanges of corresponding wheelsets pressed to inner surface of head of base rail, thus forming measuring base identifying position of base rail in points of contact of corresponding wheelsets. |
 Direction finder in one plane / 2262120Offered is a direction finder in one plane, having two antennas with identical aerial directional patterns, add-subtract converter, whose first input is connected to the output of the first antenna, two receiving devices with a common local oscillator, whose inputs are connected to the output of the first antenna, two receiving devices with a common local oscillator, whose inputs are connected to the outputs of the add-subtract converter, and angle discriminator, introduced into which, according to the invention, are the signal cut-off unit and the data correction unit, one of the inputs of the signal cut-off unit is connected to the output of the second antenna, the second input-to the first output of the data correction unit, the output of the signal cut-off unit is connected to the second input of the add-subtract converter, the inputs of the data correction unit are connected to the outputs of the receiving devices, and the other two outputs of the data correction-unit, that are not coupled to the signal cut-off unit, are connected to the inputs of the angle discriminator. |
 Device for finding position of movable robot / 2265803Device for finding position of movable robot is made for précised finding of robot's position by means of calculating time being necessary to any ultrasonic signal generated by ultrasonic signal generating aids to reach movable robot. The purpose is reached due to moment of time during which moment the radio frequency signal is generated which signal is radiated by movable robot. Distance between movable robot and charge station is calculated on the base of calculated time for achieving the robot. Angle between charge station and movable robot is calculated on the base of computed value of distance as well s on the base of preset value of distance between ultrasonic signal generating aids. |
FIELD: measurement equipment.
SUBSTANCE: invention relates to the field of determination of location of radiation sources. The specified result is achieved by the fact that at least in three mutually distanced points of reception, levels of a radio signal are measured from the source of radiation with available energy characteristics, which characterise the value of signal attenuation in the distribution channel, then, by the value of this attenuation, the distance is calculated from the object of radiation to each of the receiving stations, and using the coordinate information on location of the receiving stations, they calculate coordinates of the object of radiation. The device to determine Cartesian coordinates of the source of radiation includes at each point of reception: a non-directed antenna sensor of a half-wave vibrator; a radio receiver with an analog-digital converter at the outlet; metres of energy or amplitude of the received signal; a calculator of the distance from the source of radiation and one that combines data at receiving stations, a calculator of coordinates of the source of radiation. Coordinates of the radiation source are calculated according to formulas given in the text of invention description.
EFFECT: detection of coordinates of location of a source of radiation of available intensity in passive mode under conditions of no mutual time synchronisation of receiving stations.
2 cl, 2 dwg
The technical field to which the invention relates:
The invention relates to the field of positioning by matching in one coordinate system of three or more found distances (G01S 19/00) using radio waves (G01S 005/02) and can be used to provide a solution of navigation problems in air traffic control systems, marine navigation systems, the rescue service of ships, aircraft and other aircraft in distress. The level of technology:
Existing far-measuring methods for determining the location of objects of radio emission are based on measuring of phase or temporary delay of the wavefront at distribution of its radiation from the object to each of passive receivers [1]. Such measurements can be carried out only through the use of active query to radiation from a source with a strict time or phase synchronization between the receivers, which is a restriction on their use.
Another analogue of the invention is a difference-rangefinder method of definition of coordinates of the source of radio emission and realizing it device [2]:
The invention relates to the definition of the coordinates of the source of radio radiation (IRI) in space. The inventive as surfaces provisions Iran used the plane containing the line position of IRI, representing the intersection of two hyperbolic surfaces provisions of the relevant difference-temporal dimensions. The method is based on signal reception IRI four antennas, measuring three differences times of signal reception Iran antennas, forming the gage, post-processing the results of measurements in order to calculate the values of the parameters of the provisions of the Islamic Republic and calculating the coordinates of Iran as the point of intersection of the three planes provisions. The proposed device contains four antennas, which form three pair of measuring bases in mismatched planes, three characteristic calculator provisions of the IRI, the coordinates of the Islamic Republic in the form of the block of solving the system of linear equations and indication unit. Achievable technical result is to provide an unambiguous determination of linear coordinates of the object. Disadvantages of this method and devices as are necessary to strictly mutual timing reception points due to the necessity of measuring the time difference of the signal on each of the stations.
Third, a similar rangefinder way to determine the location of the radio station on a difference of the parish of the signal in time receiving points [3]. The invention relates to the field direction finding and can be used in the rescue service of ships, aircraft and other aircraft in distress. The purpose of the invention is increasing the accuracy of determining the location of running a radio station. This goal is achieved by the fact that at least three collection points located on the same line, measured moments of the arrival time of the signal running a radio station t a , t b and t c . Then, set the time delay of the parish of the signal at the other two points of the reception on the third. Time delay joining strength of the receiving points are calculated distance, passed radio signal, according to the formula
R i =cΔt i ,
where C is the speed of light, Dt i - lag time of the parish of the signal at the point of reception. After that calculated the distance from the reception points to the locations of the radio station by the formulas given in the description of the invention. This method also allows to make measurement location in the absence of timing between the adoptive points.
The prototype of the invention is a way to determine the location of the aircraft and the system, it handles described in [4]. On Earth there are three pulse radar stations whose coordinates are known precisely, and the planes are to be supplied . Measure three time τ 1 , t 2 , and t 3 signals between ground stations and aircraft and the appropriate distance R 1 , R 2 and R 3 . On the Central point of processing (COE) define the coordinates of the aircraft in a rectangular Cartesian coordinate system (figure 1). The system of equations linking the Cartesian coordinates of the source of radio emission and the distances measured in the present case has the following form:
; ;Adopted the following location points of the system: points 1, 2, 3 - at the vertices of an equilateral triangle with sides equal to d, point 1 and 2 - axis symmetrically relative to the start, point 3 on the Y-axis at a distance from the origin and
. The angular position of the objects of observation is defined by the azimuth of the α and the elevation angle of?. This method requires the organization of the radio channel the request-response and mutual timing points of reception.
The essence of the invention:
The purpose of the invention consists in the definition of coordinates of emitters known intensity in passive mode in conditions of absence of the relative time synchronization points of reception.
This goal is achieved by the proposed rangefinder method of definition of coordinates of emitters according to the measurements in at least three mutually distant points of the reception of radio signals, which consists in the fact that at the points of produce definition of distance from the source of the radio emission to each of the points of reception and received by distances calculated coordinates of emitters, while taking points define the intensity of the signal source, and then largest intensities signals calculate the distance from the source of the radio emission to each of the points of largest signal attenuation on the track propagation from the source of the radio emission to reception point.
Distance measurement largest signal intensity is essential sign, because this measurement does not require mutual timing of collection points and can be done in the passive mode of collection points.
This goal is responsible for determining the Cartesian coordinates of the source of radio radiation (figure 1), which includes three spatially separated omnidirectional antenna type a vibrator 1, 2 and 3; three radio 4, 5 and 6; three analog-to-digital Converter 7, 8 and 9; three meter the signal energy 10, 11 and 12; three calculator distance of 13, 14 and 15 and the evaluator of the coordinates of the source of radio emission 19. The antenna 1, radio 4, analog-to-digital Converter 7, the energy of a signal 10 and calculator distance of 13 are connected in series to form the first receiver 16; antenna 2, radio 5, analog-to-digital Converter 8, the energy of a signal 11 and computer-range 14 are connected in series to form a second receiver 17; antenna 3, radio 6, analog-to-digital Converter 9, the energy of a signal 12 and computer-range 15 are connected in series to form a third receiver 18. First, second and third receptors are located in space in such a way that they form the vertices of an equilateral triangle with sides equal basis placement d (.2). The outputs of the first, second and third of devices are connected to the respective inputs on the transmitter of the Cartesian coordinates of the source of radio emission 19.
Device works as follows: the signals from the source of the radio emission taken each antenna, 1, 2 and 3 series is amplified in the respective receivers 4, 5 and 6; are converted into digitized in an analog-to-digital converters 7, 8 and 9. The received digital sequence served on the relevant evaluators of the energy of a signal 10, 11 and 12 representing digital agreed filters. Digital sequence with the release of energy calculators signal 10, 11 and 12 are served on the relevant evaluators of the range of 13, 14 and 15, determining the distance from the source of the radio emission to the appropriate receiver by calculating the ratio of
where IZ E - known value of the energy of a signal of a radio emission source, 's APRM - effective area of a radio antenna, E PRMi - energy signal received i-m radio, corresponding to the maximum response digital matched filter, G 0 - gain antenna of a radio emission source.
Received digital values of the distances from the source of the radio emission to the first R 1 , second R 2 and the third R 3 receivers, 16, 17 and 18 are served on the computer of the Cartesian coordinates of the source of radio emission 19, calculates the location of the source signal the results of these measurements by formulas
The ratio of (1) and (2) show that for the determination of emitters known intensity you need to know gain antenna source of radio emission; the antenna area of each radio receivers and signal energy that is taken by each of the receivers. This, in turn, means that the set of distinctive features is significant, i.e. the device complies with the objectives of the invention consists in that for the determination of emitters in passive mode, don't need mutual timing receivers.
Entered in the rangefinder method of definition of coordinates of emitters according to the measurements in at least three mutually distant points of the reception of radio signals process for determining the intensity of the source signal and calculate the distance from the source of the radio emission to each of the points of largest of these intensities signals are not used in any known ranging ways of positioning. Such a set of distinctive features missing and analogues in the prototype, which proves the compliance of the proposed method criterion of «novelty».
Therefore, when analyzing the level of technology is not detected objects, having the same set of features as the claimed invention, and therefore it is new.
Inventive level of the proposed method and device supported by the fact that in the result of the search is not identified the ways and devices, with signs that match the distinctive features of the invention. All traceable directions of improvement of the ranging system, reflected in scientific and technical literature, associated with the use phase or temporary information on the measuring signals. This means that the claimed invention does not arise obvious from the prior art, and, therefore, has an inventive level.
List of figures and drawings
Figure 1 shows the block diagram of the device definition of the Cartesian coordinates of the source of radio emission, where the numbers mark: 1, 2 and 3 - three spatially separated omnidirectional antenna type a vibrator; 4, 5 and 6 - three radios; 7, 8 and 9, three analog-to-digital Converter; 10, 11 and 12 three transmitter signal energy; 13, 14 and 15 - three transmitter range, 16, 17 and 18 of the first, second and third receptors, respectively, and 19 - calculator coordinates of the source of radio emission.
Figure 2 the drawing of position in space of the first (1), second (2) and the third (3) receptors. Ibid point M identified object of radio emission, the coordinates of which you want to define.
Information supporting the possibility of the invention.
Industrial applicability of the invention defined by the possibility of the realization of its assemblies and units of the state of the art. Consider the possibility of technical implementation on the example of construction of the airfield positioning system aircraft according to the automatic dependent observations-broadcast ADS-B. fitted with ADS-B aircraft transmitting every second over the air its characteristics during the whole way. The exactly known frequency radiation power transmitters and antenna characteristics, located on Board the aircraft.
For an example of the first, second and third receiving devices can be used:
1. Omnidirectional antenna type a vibrator 1, 2 and 3 - Russian antenna company radial (10 dBi). Description: http://adsbradar.ru/content/radial-1065-1134-mhz-antenna-vertikalnava-a10-1090
2. Radio 4, 5 and 6 include preamplifiers signal, in this case it can be low-noise amplifiers on the 1090 MHz company Kuhne electronic KU LNA 1090 (30 dB). Description: http://adsbradar.ru/KU-LNA-1090-A-TM-Super-Low-Noise-Amplifier-for-Avionics. Actually signal amplifiers and frequency converters are built under the dynamic range of the ADC and do not cause technical difficulties.
3. Market analog-to-digital converters (7, 8 and 9) for the application of saturated.
4. Digital implementation calculators energy of a signal (10, 11 and 12), calculators range (13, 14 and 15) and the evaluator of the coordinates of the source of radio radiation (19) can be ensured by microprocessors in accordance with the algorithms given in the description of the invention.
Thus, the claimed invention is industrially applicable. Can be used in all industries that require locating the sources of radiation in space, such as marine ground and air radio navigation, topography, geological prospecting and .. has advantages over known, associated with the lack of necessary time synchronization points of acceptance, which leads to its technical and economic efficiency.
Literature.
1. V.S. Kondratyev, A.F. Kotov, L.N. Markov «multi-station radio systems M: Radio and Communication, 1986, .220-228.
2. Patent №2309420 EN, Application №2006103054/09, 02.02.2006, Military space Academy named A.F. Mozhaisky (EN), Publ. 27.10.2007.
3. Patent №2096800 EN, Reg. application number: 93051121 Main codes IPC: G01S 005/02 Horny V.F.
4. Radar funds for the air defense systems of the 80-ies. - Electronics abroad, 1978, №2.
1. Rangefinder method of definition of coordinates of emitters according to the measurements in at least three mutually distant points of the reception of radio signals, which consists in the fact that at the points of produce definition of distance from the source radio emission from each of the points of reception and received by distances calculated coordinates of emitters, characterized in that in a passive mode in conditions of absence of mutual timing of reception points at the points of measure the intensity of the signal source in the form of the signal energy that is determined by the maximum response matched filter, and then largest intensities signals calculate the distance from the source of the radio emission to each of the points of largest signal attenuation on the track propagation from the source of the radio emission to the point reception.
2. Device for determination of the Cartesian coordinates of the source of radio emission, containing three spatially separated omnidirectional antenna type a vibrator; three radios; three analog-to-digital Converter and calculator coordinates of the source of radio emission, and the output of each omnidirectional antenna is connected to the input of the appropriate radio, and the output of each radio is connected to the input of the corresponding analog-to-digital Converter, and the antenna and the radio and analog-to-digital converters in space in such a way that they form the vertices of an equilateral triangle with sides equal basis placement, wherein the device additionally contains three transmitter signal energy that is made in the form of digital agreed filters, and three transmitter range, the output of analog-to-digital converters radios connected to the inputs of the relevant calculators energy of a signal, and the outputs calculators energy of the signal connected to the inputs of the relevant calculators range, the output of each of calculators range is connected to the corresponding input coordinate calculator the source of the radio emission.