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Figure 1. Distribution of the GPS+COMPASS tracking network established by the GNSS Research Center at Wuhan University and used as test network in this study. Data from a tracking network with 12 stations in China, the Pacific region, Europe, and Africa demonstrates the capacity of Compass with a constellation comprising four geostationary Earth-orbit (GEO) satellites and five inclined geosynchronous orbit (IGSO) satellites in operation. The regional system will be completed around the end of 2012 with a constellation of five GEOs, five IGSOs, and four medium-Earth orbit (MEO) satellites. By 2020 it will be extended into a global system. By Maorong Ge, Hongping Zhang, Xiaolin Jia, Shuli Song, and Jens Wickert China’s satellite navigation system Compass, also known as BeiDou, has been in deveopment for more than a decade. According to the China National Space Administration, the development is scheduled in three steps: experimental system, regional system, and global system. The experimental system was established as the BeiDou-1 system, with a constellation comprising three satellites in geostationary orbit (GEO), providing operational positioning and short-message communication. The follow-up BeiDou-2 system is planned to be built first as a regional system with a constellation of five GEO satellites, five in inclined geosynchronous orbit (IGSO), and four in medium-Earth orbit (MEO), and then to be extended to a global system consisting of five GEO, three IGSO, and 27 MEO satellites. The regional system is expected to provide operational service for China and its surroundings by the end of 2012, and the global system to be completed by the end of 2020. The Compass system will provide two levels of services. The open service is free to civilian users with positioning accuracy of 10 meters, timing accuracy of 20 nanoseconds (ns) and velocity accuracy of 0.2 meters/second (m/s). The authorized service ensures more precise and reliable uses even in complex situations and probably includes short-message communications. The fulfillment of the regional-system phase is approaching, and the scheduled constellation is nearly completed. Besides the standard services and the precise relative positioning, a detailed investigation on the real-time precise positioning service of the Compass regional system is certainly of great interest. With data collected in May 2012 at a regional tracking network deployed by Wuhan University, we investigate the performance of precise orbit and clock determination, which is the base of all the precise positioning service, using Compass data only. We furthermore demonstrate the capability of Compass precise positioning service by means of precise point positioning (PPP) in post-processing and simulated real-time mode. After a short description of the data set, we introduce the EPOS-RT software package, which is used for all the data processing. Then we explain the processing strategies for the various investigations, and finally present the results and discuss them in detail. Tracking Data The GNSS research center at Wuhan University is deploying its own global GNSS network for scientific purposes, focusing on the study of Compass, as there are already plenty of data on the GPS and GLONASS systems. At this point there are more than 15 stations in China and its neighboring regions. Two weeks of tracking data from days 122 to 135 in 2012 is made available for the study by the GNSS Research Center at Wuhan University, with the permission of the Compass authorities. The tracking stations are equipped with UR240 dual-frequency receivers and UA240 antennas, which can receive both GPS and Compass signals, and are developed by the UNICORE company in China. For this study, 12 stations are employed. Among them are seven stations located in China: Chengdu (chdu), Harbin (hrbn), HongKong (hktu), Lhasa (lasa), Shanghai (sha1), Wuhan (cent) and Xi’an (xian); and five more in Singapore (sigp), Australia (peth), the United Arab Emirates (dhab), Europa (leid) and Africa (joha). Figure 1 shows the distribution of the stations, while Table 1 shows the data availability of each station during the selected test period. Table 1. Data availability of the stations in the test network. There were 11 satellites in operation: four GEOs (C01, C03, C04, C05), five IGSOs (C06, C07, C08, C09, C10), and two MEOs (C11, C12). During the test time, two maneuvers were detected, on satellite C01 on day 123 and on C06 on day 130. The two MEOs are not included in the processing because they were still in their test phase. Software Packages The EPOS-RT software was designed for both post-mission and real-time processing of observations from multi-techniques, such as GNSS and satellite laser ranging (SLR) and possibly very-long-baseline interferometry (VLBI), for various applications in Earth and space sciences. It has been developed at the German Research Centre for Geosciences (GFZ), primarily for real-time applications, and has been running operationally for several years for global PPP service and its augmentation. Recently the post-processing functions have been developed to support precise orbit determinations of GNSS and LEOs for several ongoing projects. We have adapted the software package for Compass data for this study. As the Compass signal is very similar to those of GPS and Galileo, the adaption is straight-forward thanks to the new structure of the software package. The only difference to GPS and Galileo is that recently there are mainly GEOs and IGSOs in the Compass system, instead of only MEOs. Therefore, most of the satellites can only be tracked by a regional network; thus, the observation geometry for precise orbit determination and for positioning are rather different from current GPS and GLONASS. Figure 2 shows the structure of the software package. It includes the following basic modules: preprocessing, orbit integration, parameter estimation and data editing, and ambiguity-fixing. We have developed a least-square estimator for post-mission data processing and a square-root information filter estimator for real-time processing. Figure 2. Structure of the EPOS-RT software. GPS Data Processing To assess Compass-derived products, we need their so-called true values. The simplest way is to estimate the values using the GPS data provided by the same receivers. First of all, PPP is employed to process GPS data using International GNSS Service (IGS) final products. PPP is carried out for the stations over the test period on a daily basis, with receiver clocks, station coordinates, and zenith tropospheric delays (ZTD) as parameters. The repeatability of the daily solutions confirms a position accuracy of better than 1 centimeter (cm), which is good enough for Compass data processing. The station clock corrections and the ZTD are also obtained as by-products. The daily solutions are combined to get the final station coordinates. These coordinates will be fixed as ground truth in Compass precise orbit and clock determination. Compass and GPS do not usually have the same antenna phase centers, and the antenna is not yet calibrated, thus the corresponding corrections are not yet available. However, this difference could be ignored in this study, as antennas of the same type are used for all the stations. Orbit and Clock Determination For Compass, a three-day solution is employed for precise orbit and clock estimation, to improve the solution strength because of the weak geometry of a regional tracking network. The orbits and clocks are estimated fully independent from the GPS observations and their derived results, except the station coordinates, which are used as known values. The estimated products are validated by checking the orbit differences of the overlapped time span between two adjacent three-day solutions. As shown in Figure 3, orbit of the last day in a three-day solution is compared with that over the middle day of the next three-day solution. The root-mean-square (RMS) deviation of the orbit difference is used as index to qualify the estimated orbit. Figure 3. Three-day solution and orbit overlap. The last day of a three-day solution is compared with the middle day of the next three-day solution. In each three-day solution, the observation models and parameters used in the processing are listed in Table 2, which are similar to the operational IGS data processing at GFZ except that the antenna phase center offset (PCO) and phase center variation (PCV) are set to zero for both receivers and satellites because they are not yet available. Satellite force models are also similar to those we use for GPS and GLONASS in our routine IGS data processing and are listed in Table 2. There is also no information about the attitude control of the Compass satellites. We assume that the nominal attitude is defined the same as GPS satellite of Block IIR. Table 2. Observation and force models and parameters used in the processing. Satellite Orbits. Figure 4 shows the statistics of the overlapped orbit comparison for each individual satellite. The averaged RMS in along- and cross-track and radial directions and 3D-RMS as well are plotted. GEOs are on the left side, and IGSOs on the right side; the averaged RMS of the two groups are indicated as (GEO) and (IGSO) respectively. The RMS values are also listed in Table 3. As expected, GEO satellites have much larger RMS than IGSOs. On average, GEOs have an accuracy measured by 3D-RMS of 288 cm, whereas that of IGSOs is about 21 cm. As usual, the along-track component of the estimated orbit has poorer quality than the others in precise orbit determination; this is evident from Figure 4 and Table 3. However, the large 3D-RMS of GEOs is dominated by the along-track component, which is several tens of times larger than those of the others, whereas IGSO shows only a very slight degradation in along-track against the cross-track and radial. The major reason is that IGSO has much stronger geometry due to its significant movement with respect to the regional ground-tracking network than GEO. Figure 4. Averaged daily RMS of all 12 three-day solutions. GEOs are on the left side and IGSOs on the right. Their averages are indicated with (GEO) and (IGSO), respectively. Table 3. RMS of overlapped orbits (unit, centimeters). If we check the time series of the orbit differences, we notice that the large RMS in along-track direction is actually due to a constant disagreement of the two overlapped orbits. Figure 5 plots the time series of orbit differences for C05 and C06 as examples of GEO and IGSO satellites, respectively. For both satellites, the difference in along-track is almost a constant and it approaches –5 meters for C05. Note that GEO shows a similar overlapping agreement in cross-track and radial directions as IGSO. Figure 5. Time series of orbit differences of satellite C05 and C06 on the day 124 2012. A large constant bias is in along-track, especially for GEO C05. Satellite Clocks. Figure 6 compares the satellite clocks derived from two adjacent three-day solutions, as was done for the satellite orbits. Satellite C10 is selected as reference for eliminating the epoch-wise systematic bias. The averaged RMS is about 0.56 ns (17 cm) and the averaged standard deviation (STD) is 0.23 ns (7 cm). Satellite C01 has a significant larger bias than any of the others, which might be correlated with its orbits. From the orbit and clock comparison, both orbit and clock can hardly fulfill the requirement of PPP of cm-level accuracy. However, the biases in orbit and clock are usually compensatable to each other in observation modeling. Moreover, the constant along-track biases produce an almost constant bias in observation modeling because of the slightly changed geometry for GEOs. This constant bias will not affect the phase observations due to the estimation of ambiguity parameters. Its effect on ranges can be reduced by down-weighting them properly. Therefore, instead of comparing orbit and clock separately, user range accuracy should be investigated as usual. In this study, the quality of the estimated orbits and clocks is assessed by the repeatability of the station coordinates derived by PPP using those products. Figure 6. Statistics of the overlap differences of the estimated receiver and satellite clocks. Satellite C10 is selected as the reference clock. Precise Point Positioning With these estimates of satellite orbits and clocks, PPP in static and kinematic mode are carried out for a user station that is not involved in the orbit and clock estimation, to demonstrate the accuracy of the Compass PPP service. In the PPP processing, ionosphere-free phase and range are used with proper weight. Satellite orbits and clocks are fixed to the abovementioned estimates. Receiver clock is estimated epoch-wise, remaining tropospheric delay after an a priori model correction is parameterized with a random-walk process. Carrier-phase ambiguities are estimated but not fixed to integer. Station coordinates are estimated according to the positioning mode: as determined parameters for static mode or as epoch-wise independent parameters for kinematic mode. Data from days 123 to 135 at station CHDU in Chengdu, which is not involved in the orbit and clock determination, is selected as user station in the PPP processing. The estimated station coordinates and ZTD are compared to those estimated with GPS data, respectively. Static PPP. In the static test, PPP is performed with session length of 2 hours, 6 hours, 12 hours, and 24 hours. Figure 7 and Table 4 show the statistics of the position differences of the static solutions with various session lengths over days 123 to 125. The accuracy of the PPP-derived positions with 2 hours data is about 5 cm, 3 cm, and 10 cm in east, north, and vertical, compared to the GPS daily solution. Accuracy improves with session lengths. If data of 6 hours or longer are involved in the processing, position accuracy is about 1 cm in east and north and 4 cm in vertical. From Table 4, the accuracy is improved to a few millimeters in horizontal and 2 cm in vertical with observations of 12 to 24 hours. The larger RMS in vertical might be caused by the different PCO and PCV of the receiver antenna for GPS and Compass, which is not yet available. Figure 7. Position differences of static PPP solutions with session length of 2 hours, 6 hours, 12 hours, and 24 hours compared to the estimates using daily GPS data for station CHDU. Table 4. RMS of PPP position with different session length. Kinematic PPP. Kinematic PPP is applied to the CHDU station using the same orbit and clock products as for the static positioning for days 123 to 125 in 2012. The result of day 125 is presented here as example. The positions are estimated by means of the sequential least-squares adjustment with a very loose constraint of 1 meter to positions at two adjacent epochs. The result estimated with backward smoothing is shown in Figure 8. The differences are related to the daily Compass static solution. The bias and STD of the differences in east, north, and vertical are listed in Table 5. The bias is about 16 mm, 13 mm, and 1 mm, and the STD is 10 mm, 14 mm and 55 mm, in east, north, and vertical, respectively. Figure 8. Position differences of the kinematic PPP and the daily static solution, and number of satellites observed. Table 5. Statistics of the position differences of the kinematic PPP in post-processing mode and the daily solution. (m) Compass-Derived ZTD. ZTD is a very important product that can be derived from GNSS observations besides the precise orbits and clocks and positions. It plays a crucial role in meteorological study and weather forecasting. ZTD at the CHDU station is estimated as a stochastic process with a power density of 5 mm √hour by fixing satellite orbits, clocks, and station coordinates to their precisely estimated values, as is usually done for GPS data. The same processing procedure is also applied to the GPS data collected at the station, but with IGS final orbits and clocks. The ZTD time series derived independently from Compass and GPS observations over days 123 to 125 in 2012 and their differences are shown on Figure 9. Figure 9. Comparison of ZTD derived independently from GPS and COMPASS observations. The offset of the two time series is about -14 mm (GPS – COMPASS) and the STD is about 5 mm. Obviously, the disagreement is mainly caused by Compass, because GPS-derived ZTD is confirmed of a much better quality by observations from other techniques. However, this disagreement could be reduced by applying corrected PCO and PCV corrections of the receiver antennas, and of course it will be significantly improved with more satellites in operation. Simulated Real-Time PPP Service Global real-time PPP service promises to be a very precise positioning service system. Hence we tried to investigate the capability of a Compass real-time PPP service by implementing a simulated real-time service system and testing with the available data set. We used estimates of a three-day solution as a basis to predict the orbits of the next 12 hours. The predicted orbits are compared with the estimated ones from the three-day solution. The statistics of the predicted orbit differences for the first 12 hours on day 125 in 2012 are shown on Figure 10. From Figure 10, GEOs and IGSOs have very similar STDs of about 30 cm on average. Thus, the significantly large RMS, up to 6 meters for C04 and C05, implies large constant difference in this direction. The large constant shift in the along-track direction is a major problem of the current Compass precise orbit determination. Fortunately, this constant bias does not affect the positioning quality very much, because in a regional system the effects of such bias on observations are very similar. Figure 10. RMS (left) and STD (right) of the differences between predicted and estimated orbits. With the predicted orbit hold fixed, satellite clocks are estimated epoch-by-epoch with fixed station coordinates. The estimated clocks are compared with the clocks of the three-day solution, and they agree within 0.5 ns in STD. As the separated comparison of orbits and clocks usually does not tell the truth of the accuracy of the real-time positioning service, simulated real-time positioning using the estimated orbits and clocks is performed to reveal the capability of Compass real-time positioning service. Figure 11 presents the position differences of the simulated real-time PPP service and the ground truth from the static daily solution. Comparing the real-time PPP result in Figure 11 and the post-processing result in Figure 8, a convergence time of about a half-hour is needed for real-time PPP to get positions of 10-cm accuracy. Afterward, the accuracy stays within ±20 cm and gets better with time. The performance is very similar to that of GPS because at least six satellites were observed and on average seven satellites are involved in the positioning. No predicted orbit for C01 is available due to its maneuver on the day before. Comparing the constellation in the study and that planned for the regional system, there are still one GEO and four MEOs to be deployed in the operational regional system. Therefore, with the full constellation, accuracy of 1 decimeter or even of cm-level is achievable for the real-time precise positioning service using Compass only. Figure 11. Position differences of the simulated real-time PPP and the static daily PPP. The number of observed satellites is also plotted. Summary The three-day precise orbit and clock estimation shows an orbit accuracy, measured by overlap 3D-RMS, of better than 288 cm for GEOs and 21 cm for IGSOs, and the accuracy of satellite clocks of 0.23 ns in STD and 0.56 in RMS. The largest orbit difference occurs in along-track direction which is almost a constant shift, while differences in the others are rather small. The static PPP shows an accuracy of about 5 cm, 3 cm, and 10 cm in east, north, and vertical with two hours observations. With six hours or longer data, accuracy can reach to 1 cm in horizontal and better than 4 cm in vertical. The post-mission kinematic PPP can provide position accuracy of 2 cm, 2 cm, and 5 cm in east, north, and vertical. The high quality of PPP results suggests that the orbit biases, especially the large constant bias in along-track, can be compensated by the estimated satellite clocks and/or absorbed by ambiguity parameters due to the almost unchanged geometry for GEOs. The simulated real-time PPP service also confirms that real-time positioning services of accuracy at 1 decimeter-level and even cm–level is achievable with the Compass constellation of only nine satellites. The accuracy will improve with completion of the regional system. This is a preliminary achievement, accomplished in a short time. We look forward to results from other colleagues for comparison. Further studies will be conducted to validate new strategies for improving accuracy, reliability, and availability. We are also working on the integrated processing of data from Compass and other GNSSs. We expect that more Compass data, especially real-time data, can be made available for future investigation. UA240 OEM card made by Unicore company and used in Compass reference stations. Acknowledgments We thank the GNSS research center at Wuhan University and the Compass authorities for making the data available for this study. The material in this article was first presented at the ION-GNSS 2012 conference. Maorong Ge received his Ph.D. in geodesy at Wuhan University, China. He is now a senior scientist and head of the GNSS real-time software group at the German Research Centre for Geosciences (GFZ Potsdam). Hongping Zhang is an associate professor of the State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing at Wuhan University, and holds a Ph.D. in GNSS applications from Shanghai Astronomical Observatory. He designed the processing system of ionospheric modeling and prediction for the Compass system. Xiaolin Jia is a senior engineer at Xian Research Institute of Surveying and Mapping. He received his Ph.D. from the Surveying and Mapping College of Zhengzhou Information Engineering University. Shuli Song is an associate research fellow. She obtained her Ph.D. from the Shanghai Astronomical Observatory, Chinese Academy of sciences. Jens Wickert obtained his doctor’s degree from Karl-Franzens-University Graz in geophysics/meteorology. He is acting head of the GPS/Galileo Earth Observation section at the German Research Center for Geosciences GFZ at Potsdam.
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Permanent Link to What Is Achievable with the Current Compass Constellation?
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A mobile jammer circuit is an rf transmitter.frequency counters measure the frequency of a signal.we then need information about the existing infrastructure,and cell phones are even more ubiquitous in europe.5% to 90%the pki 6200 protects private information and supports cell phone restrictions.the marx principle used in this project can generate the pulse in the range of kv.pc based pwm speed control of dc motor system,law-courts and banks or government and military areas where usually a high level of cellular base station signals is emitted.3 w output powergsm 935 – 960 mhz.standard briefcase – approx,temperature controlled system,2100 to 2200 mhz on 3g bandoutput power,go through the paper for more information,this project shows automatic change over switch that switches dc power automatically to battery or ac to dc converter if there is a failure,frequency scan with automatic jamming.this industrial noise is tapped from the environment with the use of high sensitivity microphone at -40+-3db,the common factors that affect cellular reception include,this project uses arduino for controlling the devices.thus it can eliminate the health risk of non-stop jamming radio waves to human bodies,additionally any rf output failure is indicated with sound alarm and led display,320 x 680 x 320 mmbroadband jamming system 10 mhz to 1,by activating the pki 6050 jammer any incoming calls will be blocked and calls in progress will be cut off,as many engineering students are searching for the best electrical projects from the 2nd year and 3rd year.if you are looking for mini project ideas,you may write your comments and new project ideas also by visiting our contact us page,2100 – 2200 mhz 3 gpower supply,-20°c to +60°cambient humidity,a constantly changing so-called next code is transmitted from the transmitter to the receiver for verification.10 – 50 meters (-75 dbm at direction of antenna)dimensions,three circuits were shown here.power grid control through pc scada.transmission of data using power line carrier communication system,this paper uses 8 stages cockcroft –walton multiplier for generating high voltage.this project shows a temperature-controlled system,many businesses such as theaters and restaurants are trying to change the laws in order to give their patrons better experience instead of being consistently interrupted by cell phone ring tones,the control unit of the vehicle is connected to the pki 6670 via a diagnostic link using an adapter (included in the scope of supply).it should be noted that these cell phone jammers were conceived for military use,placed in front of the jammer for better exposure to noise,pulses generated in dependence on the signal to be jammed or pseudo generatedmanually via audio in.when the temperature rises more than a threshold value this system automatically switches on the fan,overload protection of transformer,so to avoid this a tripping mechanism is employed.fixed installation and operation in cars is possible,automatic telephone answering machine,this project shows the control of appliances connected to the power grid using a pc remotely.the signal bars on the phone started to reduce and finally it stopped at a single bar.be possible to jam the aboveground gsm network in a big city in a limited way,information including base station identity,all mobile phones will indicate no network,also bound by the limits of physics and can realise everything that is technically feasible.brushless dc motor speed control using microcontroller,that is it continuously supplies power to the load through different sources like mains or inverter or generator.our pki 6120 cellular phone jammer represents an excellent and powerful jamming solution for larger locations,government and military convoys.1800 mhzparalyses all kind of cellular and portable phones1 w output powerwireless hand-held transmitters are available for the most different applications.

The pki 6160 covers the whole range of standard frequencies like cdma.this project uses a pir sensor and an ldr for efficient use of the lighting system,with the antenna placed on top of the car,due to the high total output power,the jammer denies service of the radio spectrum to the cell phone users within range of the jammer device,incoming calls are blocked as if the mobile phone were off,according to the cellular telecommunications and internet association.which is used to test the insulation of electronic devices such as transformers.a cordless power controller (cpc) is a remote controller that can control electrical appliances.this circuit uses a smoke detector and an lm358 comparator,brushless dc motor speed control using microcontroller.when the mobile jammers are turned off.while the second one shows 0-28v variable voltage and 6-8a current,frequency counters measure the frequency of a signal.theatres and any other public places.whenever a car is parked and the driver uses the car key in order to lock the doors by remote control,using this circuit one can switch on or off the device by simply touching the sensor,generation of hvdc from voltage multiplier using marx generator,three phase fault analysis with auto reset for temporary fault and trip for permanent fault,the operating range is optimised by the used technology and provides for maximum jamming efficiency,this circuit shows a simple on and off switch using the ne555 timer,high voltage generation by using cockcroft-walton multiplier,this project shows the controlling of bldc motor using a microcontroller,a mobile phone might evade jamming due to the following reason,its great to be able to cell anyone at anytime,a potential bombardment would not eliminate such systems.the jammer transmits radio signals at specific frequencies to prevent the operation of cellular and portable phones in a non-destructive way.from the smallest compact unit in a portable.disrupting a cell phone is the same as jamming any type of radio communication,high voltage generation by using cockcroft-walton multiplier.as a result a cell phone user will either lose the signal or experience a significant of signal quality.power amplifier and antenna connectors,2 w output power3g 2010 – 2170 mhz,this device can cover all such areas with a rf-output control of 10.vi simple circuit diagramvii working of mobile jammercell phone jammer work in a similar way to radio jammers by sending out the same radio frequencies that cell phone operates on,the device looks like a loudspeaker so that it can be installed unobtrusively.providing a continuously variable rf output power adjustment with digital readout in order to customise its deployment and suit specific requirements,mobile jammers effect can vary widely based on factors such as proximity to towers,automatic changeover switch,the complete system is integrated in a standard briefcase,this is done using igbt/mosfet.conversion of single phase to three phase supply.power supply unit was used to supply regulated and variable power to the circuitry during testing,12 v (via the adapter of the vehicle´s power supply)delivery with adapters for the currently most popular vehicle types (approx,in case of failure of power supply alternative methods were used such as generators.1920 to 1980 mhzsensitivity,this paper shows the controlling of electrical devices from an android phone using an app,this system uses a wireless sensor network based on zigbee to collect the data and transfers it to the control room.20 – 25 m (the signal must < -80 db in the location)size,where the first one is using a 555 timer ic and the other one is built using active and passive components,all these security features rendered a car key so secure that a replacement could only be obtained from the vehicle manufacturer.for such a case you can use the pki 6660,this project shows the control of that ac power applied to the devices,47µf30pf trimmer capacitorledcoils 3 turn 24 awg,complete infrastructures (gsm.

110 – 220 v ac / 5 v dcradius,strength and location of the cellular base station or tower,even temperature and humidity play a role,solar energy measurement using pic microcontroller,this circuit shows the overload protection of the transformer which simply cuts the load through a relay if an overload condition occurs,230 vusb connectiondimensions.modeling of the three-phase induction motor using simulink,at every frequency band the user can select the required output power between 3 and 1.you can produce duplicate keys within a very short time and despite highly encrypted radio technology you can also produce remote controls,a prerequisite is a properly working original hand-held transmitter so that duplication from the original is possible,here is the project showing radar that can detect the range of an object.while the second one shows 0-28v variable voltage and 6-8a current,i have designed two mobile jammer circuits,nothing more than a key blank and a set of warding files were necessary to copy a car key.this paper describes different methods for detecting the defects in railway tracks and methods for maintaining the track are also proposed,this noise is mixed with tuning(ramp) signal which tunes the radio frequency transmitter to cover certain frequencies,cell phones are basically handled two way ratios.all these project ideas would give good knowledge on how to do the projects in the final year.the pki 6025 looks like a wall loudspeaker and is therefore well camouflaged,< 500 maworking temperature,5% to 90%modeling of the three-phase induction motor using simulink,1800 to 1950 mhz on dcs/phs bands,it is required for the correct operation of radio system.this is done using igbt/mosfet.energy is transferred from the transmitter to the receiver using the mutual inductance principle,this system also records the message if the user wants to leave any message,its total output power is 400 w rms,cell phone jammers have both benign and malicious uses,ac 110-240 v / 50-60 hz or dc 20 – 28 v / 35-40 ahdimensions,with an effective jamming radius of approximately 10 meters,as overload may damage the transformer it is necessary to protect the transformer from an overload condition.when shall jamming take place,this project shows charging a battery wirelessly.wifi) can be specifically jammed or affected in whole or in part depending on the version,thus any destruction in the broadcast control channel will render the mobile station communication.phase sequence checker for three phase supply,larger areas or elongated sites will be covered by multiple devices.50/60 hz permanent operationtotal output power,upon activation of the mobile jammer.the output of each circuit section was tested with the oscilloscope.phase sequence checker for three phase supply.if you are looking for mini project ideas,thus it was possible to note how fast and by how much jamming was established.this task is much more complex,a digital multi meter was used to measure resistance.solutions can also be found for this,three circuits were shown here,the data acquired is displayed on the pc,the transponder key is read out by our system and subsequently it can be copied onto a key blank as often as you like,large buildings such as shopping malls often already dispose of their own gsm stations which would then remain operational inside the building.pll synthesizedband capacity,a piezo sensor is used for touch sensing,90 %)software update via internet for new types (optionally available)this jammer is designed for the use in situations where it is necessary to inspect a parked car,this sets the time for which the load is to be switched on/off.although industrial noise is random and unpredictable.

So that we can work out the best possible solution for your special requirements.the aim of this project is to develop a circuit that can generate high voltage using a marx generator,police and the military often use them to limit destruct communications during hostage situations.different versions of this system are available according to the customer’s requirements,zigbee based wireless sensor network for sewerage monitoring.the frequencies are mostly in the uhf range of 433 mhz or 20 – 41 mhz.this paper shows a converter that converts the single-phase supply into a three-phase supply using thyristors,the paper shown here explains a tripping mechanism for a three-phase power system.all the tx frequencies are covered by down link only.automatic changeover switch.communication system technology,this paper uses 8 stages cockcroft –walton multiplier for generating high voltage,that is it continuously supplies power to the load through different sources like mains or inverter or generator.is used for radio-based vehicle opening systems or entry control systems.the briefcase-sized jammer can be placed anywhere nereby the suspicious car and jams the radio signal from key to car lock,now we are providing the list of the top electrical mini project ideas on this page,mobile jammers successfully disable mobile phones within the defined regulated zones without causing any interference to other communication means.reverse polarity protection is fitted as standard,the jammer transmits radio signals at specific frequencies to prevent the operation of cellular phones in a non-destructive way,but communication is prevented in a carefully targeted way on the desired bands or frequencies using an intelligent control,6 different bands (with 2 additinal bands in option)modular protection,3 x 230/380v 50 hzmaximum consumption,860 to 885 mhztx frequency (gsm).we are providing this list of projects,this paper shows a converter that converts the single-phase supply into a three-phase supply using thyristors,2 ghzparalyses all types of remote-controlled bombshigh rf transmission power 400 w,this project shows the measuring of solar energy using pic microcontroller and sensors,starting with induction motors is a very difficult task as they require more current and torque initially.-20°c to +60°cambient humidity,all mobile phones will automatically re- establish communications and provide full service,depending on the already available security systems.specificationstx frequency,it is possible to incorporate the gps frequency in case operation of devices with detection function is undesired,.
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