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Its Algorithms and Performance The authors test three mass-market design drivers on a chip developed expressly for a new role as a combined GPS and Galileo consumer receiver: the time-to-first-fix for different C/N0, for hot, warm, and cold start, and for different constellation combinations; sensitivity in harsh environments, exploiting a simulated land mobile satellite multipath channel and different user dynamics; and power consumption strategies, particularly duty-cycle tracking. By Nicola Linty, Paolo Crosta, Philip G. Mattos, and Fabio Pisoni The two main GNSS receiver market segments, professional high-precision receivers and mass-market/consumer receivers, have very different structure, objectives, features, architecture, and cost. Mass-market receivers are produced in very high volume — hundreds of millions for smartphones and tablets — and sold at a limited price, and in-car GNSS systems represent a market of tens of millions of units per year. The reason for these exploding markets can be found not only in the improvements in electronics and integration, but also in the increasing availability of new GNSS signals. In coming years, with Galileo, QZSS, BeiDou, GPS-L1C, and GLONASS-CDMA all on the way, the silicon manufacturer must continue the path towards the fully flexible multi-constellation mass-market receiver. Mass-market receivers feature particular signal processing techniques, different from the acquisition and tracking techniques of standard GNSS receivers, in order to comply with mobile and consumer devices’ resources and requirements. However, a limited documentation is present in the open literature concerning consumer devices’ algorithms and techniques; besides a few papers, all the know-how is protected by patents, held by the main manufacturers, and mainly focused on the GPS L1 C/A signal. We investigate and prove the feasibility of such techniques by semi-analytical and Monte Carlo simulations, outlining the estimators sensitivity and accuracy, and by tests on real Galileo IOV signals. To understand, analyze, and test this class of algorithms, we implemented a fully software GNSS receiver, running on a personal computer. It can process hardware- and software-simulated GPS L1 C/A and Galileo E1BC signals, as well as real signals, down-converted at intermediate frequency (IF), digitalized and stored in memory by a front-end/bit grabber; it can also output standard receiver parameters: code delay, Doppler frequency, carrier-to-noise power density ratio (C/N0), phase, and navigation message. The software receiver is fully configurable, extremely flexible, and represents an important tool to assess performance and accuracy of selected techniques in different circumstances. Code-Delay Estimation The code-delay estimation is performed in the software receiver by a parallel correlation unit, giving as output a multi-correlation with a certain chip spacing. This approach presents some advantages, mostly the fact that the number of correlation values that can be provided is thousands of times greater, compared to a standard receiver channel. Use of multiple correlators increases multipath-rejection capabilities, essential features in mass-market receivers, especially for positioning in urban scenarios. The multi-correlation output is exploited to compute the received signal code delay with an open-loop strategy and then to compute the pseudorange. In the simulations performed, the multi-correlation has a resolution of 1/10 of a chip, which is equivalent to 30 meters for the signals in question; to increase the estimate accuracy, Whittaker-Shannon interpolation is performed on the equally spaced points of the correlation function belonging to the correlation peak. The code-delay estimate accuracy is reported in Figures 1 and 2. The results are obtained with Monte Carlo simulations on simulated GNSS signals, with sampling frequency equal to 16.3676 MHz. In particular, a GPS L1 C/A signal is considered, affected by constant Doppler frequency equal to zero for the observation period, to avoid the effect of dynamics. The figures show the standard deviation of the code estimation error, that is, the difference between the estimated code delay and the true one, expressed in meters (pseudorange error standard deviation) for different values of C/N0. To evaluate the quality of the results, the theoretical delay locked loop (DLL) tracking jitter is plotted for comparison, as where Bn is the code loop noise bandwidth, Rc is the chipping rate, Bfe is the single sided front-end bandwidth, Tc is the coherent integration time, and c is the speed of light. In the two figures, the red curve shows the theoretical tracking jitter for a DLL, which can be considered as term of comparison for code-delay estimation. To correlate the results, a E-L spacing equal to D = 0.2 chip is chosen, and the code-delay error values of the software receiver simulation are filtered with a moving average filter. By averaging 0.5 seconds of data (for example, L = 31 values spaced 16 milliseconds), an equivalent closed-loop bandwidth of about 1 Hz can be obtained: In particular, in Figure 1, a coherent integration time equal to 1 millisecond (ms) and 16 non-coherent sums are considered, while in Figure 2 a coherent integration time equal to 4 ms and 16 non-coherent sums, spanning a total time T=64 ms, are considered. In both cases, the software receiver results are extremely good for high C/N0. The code-delay error estimate is slightly higher than its equivalent in the DLL formulation. The open-loop estimation error notably increases in the first case below 40 dB-Hz due to strong outliers, whose probability of occurrence depends on the C/N0. In fact, this effect is smoothed in the second case, where the coherent integration time is four times larger, thus improving the signal-to-noise ratio. Figure 1. Comparison between code delays estimation accuracy, Tc=1 ms , T=16 ms, B=1 Hz, D=0.2 chip. Figure 2. Comparison between code delays estimation accuracy, Tc=4 ms, T=64 ms, B=1 Hz, D=0.2 chip. Nevertheless, the comparison between open loop multi-correlation approach and closed loop DLL is difficult and approximate, because the parameters involved are different and the results are only qualitative. Doppler Frequency Estimation In the particular case of the software receiver developed here, the residual Doppler frequency affecting the GNSS signal is estimated by means of a maximum likelihood estimator (MLE) on a snapshot of samples, exploiting open-loop strategy. In fact, despite the higher standard deviation of the frequency error (jitter), open-loop processing offers improved tracking sensitivity, higher tracking robustness against fading and interference, and better stability when increasing the coherent integration time. In addition, the open-loop approach does not require the design of loop filters, avoiding problems with loop stability. A certain number of successive correlator values, computed in the multiple correlations block, are combined in a fast Fourier transform (FFT) and interpolated. Figure 3 shows the root mean square error (RMSE) of the frequency estimate versus signal C/N0, obtained collecting 16 coherent accumulations of 4 ms of a Galileo E1B signal, then computing a 16 points FFT spanning a time interval of 64 ms, and finally refining the result with an interpolation technique. Three different curves are shown, corresponding respectively to: the RMSE derived from simulations, carried out with GNSS data simulated with the N-FUELS signal generator; a semi-analytical estimation, exploiting the same algorithm; the Cramer-Rao lower bound (CRLB) for frequency estimation, shown as where fs is the sampling frequency. Figure 3. Doppler frequency estimate RMSE versus C/N0 in super-high resolution with T=64 ms, comparison between theoretical and simulated results. A well-known drawback is the so-called threshold effect. Below a certain C/N0, the frequency estimate computed with MLE suffers from an error, and the RMSE increases with respect to the CRLB. Mass-Market Design Drivers Once we have analyzed the features of some mass-market algorithms with a software receiver, we can move toward the performance of a real mass-market device, to compare results and confirm improvements brought by the new Galileo signals, so far mainly known from a theoretical point of view. A recent survey identified three main drivers in the design of a mass-market receiver, coming directly from user needs, and solvable in different ways. Time-to-first-fix (TTFF) corresponds to how fast a position, velocity, and time (PVT) solution is available after the receiver is powered on, that is, the time that a receiver takes to acquire and track a minimum of four satellites, and to obtain the necessary information from the demodulated navigation data bits or from other sources. Capability in hostile environments, for example while crossing an urban canyon or when hiking in a forest, is measured in terms of sensitivity. It can be verified by decreasing the received signal strength and/or adding multipath models. Power consumption of the device. GNSS chipset is in general very demanding and can produce a not-negligible battery drain. We analyzed these three drivers with a commercial mass-market receiver and with the software receiver. Open-Sky TTFF Analysis TTFF depends on the architecture of the receiver, for example the number of correlators or the acquisition strategy, on the availability of assistance data, such as rough receiver position and time or space vehicles’ (SV) ephemeris data, and on the broadcast navigation message structure. Some receivers, like the one used here for testing, embed an acquisition engine that can be activated on request and assures a low acquisition time; moreover, they implement ephemeris extension. In contrast, other consumer receiver manufacturers exploit a baseband-configurable processing unit, similar to the one implemented in the software receiver, with thousands of parallel correlators generating a multi-correlator output with configurable spacing, depending on the accuracy required. By selecting an appropriate number of correlators, depending on the available assistance data and on the accuracy required, the TTFF consequently varies. We assessed the performance of the receiver under test for different C/N0, for hot, warm, and cold start, and for different constellation combinations, exploiting hardware-simulated GNSS data. Good results are achieved, especially when introducing Galileo signals. Figure 4 reports the hot-start TTFF for different C/N0 values in the range 25–53 dB-Hz, computed using the receiver. The receiver, connected to a signal generator, is configured in dual-constellation mode (GPS and Galileo) and carries out 40 TTFF trials, with a random delay between 15 and 45 seconds. In a standard additive white Gaussian noise (AWGN) channel and in hot-start conditions, the results mainly depend on the acquisition strategy and on the receiver availability of correlators and acquisition engines. In an ideal case with open-sky conditions and variable C/N0, the introduction of a second constellation only slightly improves the TTFF performance; this result cannot be generalized since it mainly depends on the acquisition threshold of the receiver, which can change using signals of different constellations. In real-world conditions, the situation can vary. Figure 4. Hot start TTFF for Galileo+GPS configuration versus C/N0 using the test receiver. Cold Start. Secondly, we analyze TTFF differences due to the different structure of GPS and Galileo navigation messages. The I/NAV message of the Galileo E1 signal and the data broadcast by GPS L1 C/A signals contain data related to satellite clock, ephemeris, and GNSS time: parameters relevant to the position fix since they describe the position of the satellite in its orbit, its clock error, and the transmission time of the received message. Table 1 shows some results in the particular case of cold start, with an ideal open-sky AWGN scenario. The TTFF is significantly lower when using Galileo satellites: while the mean TTFF when tracking only GPS satellites is equal to about 31.9 seconds (s), it decreases to 24.7 s when considering only Galileo satellites, and to 22.5 s in the case of dual constellation. Similarly, the minimum and maximum TTFF values are lower when tracking Galileo satellites. The 95 percent probability values confirm the theoretical expectations. Again, in the ideal case with open-sky conditions, the results with two constellations are quite similar to the performance of the signal with faster TTFF. However, in non-ideal conditions, use of multiple constellations represents a big advantage and underlines the importance of developing at least dual-constellation mass-market receivers. Table 1. Comparison between TTFF (in seconds) in cold start for different constellation combinations. Furthermore, it is interesting to analyze in more detail the case of a GPS and Galileo joint solution. GPS and Galileo system times are not synchronized, but differ by a small quantity, denoted as the GPS-Galileo Time Offset (GGTO). When computing a PVT solution with mixed signals, three solutions are possible: to estimate it as a fifth unknown, to read it from the navigation message, or to use pre-computed value. In the first case it is not necessary to rely on the information contained in the navigation message, eventually reducing the TTFF. However, five satellites are required to solve the five unknowns, and this is not always the case in urban scenarios or harsh environments, as will be proved below. On the contrary, in the second case, it is necessary to obtain the GGTO information from the navigation message, and since it appears only once every 30 seconds, in the worst case it is necessary to correctly demodulate 30 seconds of data. Both approaches show benefits and disadvantages, depending on the environment. The receiver under test exploits the second solution: in this case, it is possible to see an increase in the average TTFF when using a combination of GPS and Galileo, due to the demodulation of more sub-frames of the broadcast message. Sensitivity: Performance in Harsh Environments Harsh environment is the general term used to describe those scenarios in which open sky and ideal propagation conditions are not fulfilled. It can include urban canyons, where the presence of high buildings limits the SV visibility and introduces multipath; denied environments, where unintentional interference may create errors in the processing; or sites where shadowing of line-of-sight (LoS) path is present, for example due to trees, buildings, and tunnels. In these situations it is necessary to pay particular attention to the signal-processing stage; performance is in general reduced up to the case in which the receiver is not able to compute a fix. A first attempt to model such an environment has been introduced in the 3GPP standard together with the definition of A-GNSS minimum performance requirements for user equipment supporting other A-GNSSs than GPS L1 C/A, or multiple A-GNSSs which may or may not include GPS L1 C/A. The standard test cases support up to three different constellations; in dual-constellation case it foresees three satellites in view for each constellation with a horizontal dilution of precision (HDOP) ranging from 1.4 to 2.1. To perform TTFF and sensitivity tests applying the 3GPP standard test case, we configured a GNSS simulator scenario with the following characteristics, starting from the nominal constellation: Six SVs: three GPS (with PRN 6,7, 21) and three Galileo (with code number 4, 11, 23); HDOP in the range 1.4 – 2.1; nominal power as per corresponding SIS-ICD; user motion, with a heading direction towards 90° azimuth, at a constant speed of 5 kilometers/hour (km/h). In addition to limiting the number of satellites, we introduced a narrowband multipath model. The multi-SV two-states land mobile satellite (LMS) model simulator generated fading time series representative of an urban environment. The model includes two states: a good state, corresponding to LOS condition or light shadowing; a bad state, corresponding to heavy shadowing/blockage. Within each state, a Loo-distributed fading signal is assumed. It includes a slow fading component (lognormal fading) corresponding to varying shadowing conditions of the direct signal, and a fast fading component due to multipath effects. In particular, the last version of the two-state LMS simulator is able to generate different but correlated fading for each single SV, according to its elevation and azimuth angle with respect to the user position: the angular separation within satellites is crucial, since it affects the correlation of the received signals. This approach is based on a master–slave concept, where the state transitions of several slave satellites are modeled according to their correlation with one master satellite, while neglecting the correlation between the slave satellites. The nuisances generated are then imported in the simulator scenario, to timely control phase and amplitude of each simulator channel. Using this LMS scenario, the receiver’s performance in harsh environments has been then verified with acquisition (TTFF) and tracking tests. The TTFF was estimated with about 50 tests, in hot, warm, and cold start, first using both GPS and Galileo satellites, and then using only one constellation. In the second case only the 2D fix is considered, since, according to the scenario described, at maximum three satellites are in view. Table 2 reports the results for the dual-constellation case: in hot start the average TTFF is about 8 s, and it increases to 36 s and 105 s respectively for the warm and cold cases. Clearly the results are much worse than in the case reported earlier of full open-sky AWGN conditions. In this scenario only six satellites are available at maximum; moreover, the presence of multipath and fading affects the results, and they exhibit a larger variance, because of the varying conditions of the scenario. Table 2. TTFF (in seconds) exploiting GPS and Galileo constellations in harsh environments. Table 3 shows similar results, but for the GPS-only case. In this case the receiver was configured to track only GPS satellites. The mean TTFF increases both in the hot and in the warm case, whereas in cold start it is not possible compute a 2D fix with only three satellites; the ambiguity of the solution cannot be solved if an approximate position solution is not available. It may seem unfair to compare a scenario with three satellites and one with six satellites. However, it can be assumed that this is representative of what happens in limited-visibility conditions, where a second constellation theoretically doubles the number of satellites in view. Table 3. TTFF (in seconds) exploiting only GPS constellations in harsh environments. The results confirm the benefits of dual-constellation mass-market receivers in harsh environments where the number of satellites in view can be very low. Making use of the full constellation of Galileo satellites will allow mass-market receivers to substantially increase performances in these scenarios. Tracking.We carried out a 30-minute tracking test with both the receiver and the software receiver model. Both were able to acquire the six satellites and to track them, even with some losses of lock (LoLs) due to fading and multipath reflections. Figure 5 shows the number of satellites in tracking state in the receiver at every second, while Figure 6 shows the HDOP as computed by the receiver. When all six satellites are in tracking state, the HDOP lies in the range 1.4 – 2.1, as defined in the simulation scenario; on the contrary, as expected, in correspondence with a LoL it increases. Figure 6. HDOP computed by the test receiver in the Multi-SV LMS simulation. Figure 7 compares the signal power generated by the simulator and the power estimated by the receiver, in the case of GPS PRN 7 and Galileo code number 23. This proves the tracking capability of the receiver also for high sensitivity. To deal with low-power signals, the integration time is extended both for GPS and for Galileo, using the pilot tracking mode in the latter case. Figure 7. C/N0 estimate computed by the receiver in harsh environments and compared with the signal power. Figures 8 and 9 show respectively the position and the velocity solution. In the first case latitude, longitude, and altitude are plotted, while in the second case the receiver speed estimate in km/h is reported. Figure 8. Test receiver position solution in LMS scenario. Figure 9. Test receiver velocity solution in LMS scenario. In this framework it is possible to evaluate the advantages and disadvantages of using the broadcast GGTO when computing a mixed GPS and Galileo position. When the LMS channel conditions are good, all six SVs in view are in tracking state, as shown in Figure 5. However, when the fading becomes important, the number is reduced to only two satellites. If the receiver is designed to extract the GGTO from the navigation message, then a PVT solution is possible also when only four satellites are in tracking state, that is for 90 percent of the time in this specific case. On the contrary, if the GGTO has to be estimated, one more satellite is required, and this condition is satisfied only 57 percent of the time, strongly reducing the probability of having a fix. Nevertheless, estimating the GGTO requires the correct demodulation of the navigation message, and this is possible only if the signal is good enough for a sufficient time. Figure 5. Number of satellites tracked by the test receiver in the Multi-SV LMS simulation. Power-Saving Architectures The final driver for mass-market receivers design is represented by power consumption. Particularly for chips suited for portable devices running on batteries, power drain represents one of the most important design criteria. To reduce at maximum the power consumption, chip manufacturers have adopted various solutions. Most are based on the concept that, contrarily to a classic GNSS receiver, a mass-market receiver is not required to constantly compute a PVT solution. In fact, most of the time, GNSS chipsets for consumer devices are only required to keep updated information on approximate time and position and to download clock corrections and ephemeris data with a proper time rate, depending on the navigation message type and the adopted extended ephemeris algorithm. Then, when asked, the receiver can quickly provide a position fix. By reducing the computational load of the device during waiting mode, power consumption is reduced proportionally. To better understand advantages and disadvantages of power saving techniques, some of them have been studied and analyzed in detail. In particular, the algorithm implemented in the software receiver model is based on two different receiver states: an active state, in which all receiver parts are activated, as in a standard receiver, and a sleep state, where the receiver is not operating at all. In the sleep state, the GNSS RF module, GNSS baseband, and digital signal processor core are all switched off. By similarity to a square wave, these types of tracking algorithms are also called duty-cycle (DC) algorithms. Exploiting the software approach’s flexibility, we can test the effect of two important design parameters: sleep period length; minimum active period length. Their setting is not trivial and depends on the channel conditions, on the signal strength, on the number of satellites in view, on the user dynamics, and finally on the required accuracy. In the software receiver simulations performed, the active mode length is fixed to 64 ms: the receiver collects 16 correlation values with coherent integration time equal to 4 ms, to perform frequency estimation as described above. Then it switches to sleep state for 936 ms, until a real-time clock (RTC) wake-up initiates the next full-power state. In this way a fix is available at the rate of 1 s, as summarized in Figure 10. However, there are some situations where the receiver may stay in full-power mode, for example during the initialization phase, to collect important data from the navigation message, such as the ephemeris, and to perform RTC calibration. Figure 10. Duty cycle tracking pattern in the software receiver simulations. There are benefits of using this approach coupled to Galileo signals: the main impact is the usage of the pilot codes. Indeed, a longer integration time allows reducing the active period length, which most impacts the total power consumption, being usually performed at higher repetition rate. Some simulations were carried out to assess the performance of DC algorithms in the software receiver. While in hardware implementations the direct benefit is the power computation, in a software implementation it is not possible to see such an improvement. The reduced power demand is translated into a shorter processing time for each single-processing channel. The DC approach can facilitate the implementation of a real-time or quasi-real-time software receiver. The main drawback of using techniques based on DC tracking is the decrease of the rate of observables and PVT solution. However, this depends on the application; for some, a solution every second is more than enough. Real-Signal Results On March 12, 2013, for the first time  the four Galileo IOV satellites were broadcasting a valid navigation message at the same time. From 9:02 CET, all the satellites were visible at ESTEC premises, and the first position fix of latitude, longitude, and altitude took place at the TEC Navigation Laboratory at ESTEC (ESA) in Noordwijk, the Netherlands. At the same time, we were able to acquire, track, and compute one of the first Galileo-only mobile navigation solutions, using the receiver under test. Thanks to its small size and portability, it was installed on a mobile test platform, embedded in ESA’s Telecommunications and Navigation Testbed vehicle. Using a network connection, we could follow, from the Navigation Lab, the real-time position of the van moving around ESTEC. Figure 11 shows the van’s track, obtained by post processing NMEA data stored by the receiver evaluation board. The accuracy achieved in these tests met all the theoretical expectations, taking into account the limited infrastructure deployed so far. In addition, the results obtained with the receiver have to be considered preliminary, since its firmware supporting Galileo was in an initial test phase (for example, absence of a proper ionospheric model, E1B-only tracking). Figure 11. Galileo-only mobile fix, computed on March 12, 2013. Conclusions Analysis of a receiver’s test results confirms the theoretical benefits of Galileo OS signals concerning TTFF and sensitivity. Future work will include the evolution of the software receiver model and a detailed analysis of power-saving tracking capabilities, with a comparison of duty-cycle tracking techniques in open loop and in closed loop. Acknowledgments This article reflects solely the authors’ views and by no means represents official European Space Agency or Galileo views. The article is based on a paper first presented at ION GNSS+ 2013. Research and test campaigns related to this work took place in the framework of the ESA Education PRESTIGE programme, thanks to the facilities provided by the ESA TEC-ETN section. The LMS multipath channel model was developed in the frame of the MiLADY project, funded by the ARTES5.1 Programme of the ESA Telecommunications and Integrated Applications Directorate. Manufacturers The tests described here used the STMicroelectronics Teseo II receiver chipset and a Spirent signal simulator. Nicola Linty is a Ph.D. student in electronics and telecommunications at Politecnico di Torino. In 2013 he held an internship at the European Space Research and Technology Centre of ESA. Paolo Crosta is a radio navigation system engineer at the ESA TEC Directorate where he provides support to the EGNOS and Galileo programs. He received a MSc degree in telecommunications engineering from the University of Pisa. Philip G. Mattos received an external Ph.D. on his GPS work from Bristol University. He leads the STMicroelectronics team on L1C and BeiDou implementation, and the creation of totally generic hardware that can handle even future unknown systems. Fabio Pisoni has been with the GNSS System Team at STMicroelectronics since 2009. He received a master’s degree in electronics from Politecnico di Milano, Italy.

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Edac ea10523c-120 ac adapter 12vdc 5a used 2.5 x 5.5 x 11mm.konica minolta bc-600 4.2v dc 0.8a camera battery charger 100-24,hp hstnn-ha01 ac adapter 19vdc 7.1a 135w used 5x7.4mm,energizer fps005usc-050050 white ac adapter 5vdc 0.5a used 2x4.92p1157 replacement ac adapter 20v dc 3.25a ibm laptop power sup,the jamming success when the mobile phones in the area where the jammer is located are disabled.canon k30216 ac adapter 24v 0.5a battery charger,energizer fm050012-us ac adapter 5v dc 1.2a used 1.7x4x9.7mm rou.l.t.e. lte50e-s2-1 ac adapter 12v dc 4.17a 50w power supply for,fujitsu sec80n2-19.0 ac adapter 19vdc 3.16a used -(+)- 3x5.5mm 1,hjc hasu11fb ac adapter 12vdc 4a -(+) 2.5x5.5mm used 100-240vac,digipower tc-500n solutions world travel nikon battery charge,huawei hw-050100u2w ac adapter travel charger 5vdc 1a used usb p,failure to comply with these rules may result in,phase sequence checking is very important in the 3 phase supply,axis a41312 ac adapter 12vdc 1100ma used -(+) 2.5x5.5x13mm 90° r,3com sc102ta1503b03 ac adapter 15vdc 1.2a power supply,li shin lse0107a1240 ac adapter 12vdc 3.33a used 2x5.5mm 90° rou.shenzhen sun-1200250b3 ac adapter 12vdc 2.5a used -(+) 2x5.5x12m.hoioto ads-45np-12-1 12036g ac adapter 12vdc 3a used -(+) 2x5.5x,we only describe it as command code here,ab41-060a-100t ac adapter 5vdc 1a.

Religious establishments like churches and mosques,or 3) imposition of a daily fine until the violation is ….microsoft dpsn-10eb xbox 360 quick charge kit.griffin p2275 charger 5vdc 2.1a from 12vdc new dual usb car adap,sony ac-64n ac adapter 6vdc 500ma used -(+) 1.5x4x9.4mm round ba,ad 9/8 ac dc adapter 9v 800ma -(+)- 1.2x3.8mm 120vac power suppl.bogen rf12a ac adapter 12v dc 1a used power supply 120v ac ~ 60h,fisher-price na060x010u ac adapter 6vdc 100ma used 1.3x3.3mm.sony vgp-ac19v35 ac adapter 19.5v dc 4.7a laptop power supply,canon cb-2lv g battery charger 4.2vdc 0.65a used ite power suppl.ea10362 ac adapter 12vdc 3a used -(+) 2.5x5.5mm round barrel,sony ac-fd008 ac adapter 18v 6.11a 4 pin female conector.4.6v 1a ac adapter used car charger for nintendo 3ds 12v.hoover series 300 ac adapter 5.9vac 120ma used 2x5.5mm round bar,delta electronics, inc. adp-15gh b ac dc adapter 5v 3a power sup.component telephone u060030d12 ac adapter 6vdc 300ma power suppl,verifone nu12-2120100-i1 ac adapter 12v 1a used -(+)- 2.5 x5.5mm.altec lansing acs340 ac adapter 13vac 4a used 3pin 10mm mini din,finecom ky-05036s-12 ac adpter 12vdc 5v dc 2a 5pin 9mm mini din,which broadcasts radio signals in the same (or similar) frequency range of the gsm communication,15 to 30 metersjamming control (detection first),liteon pa-1750-02 ac adapter 19vdc 3.95a used 1.8 x 5.4 x 11.1 m.

Complete infrastructures (gsm,motorola spn5404aac adapter 5vdc 550ma used mini usb cellphone.dve dvr-0920ac-3508 ac adapter 9vac 200ma used 1.1x3.8x5.9mm rou,iii relevant concepts and principlesthe broadcast control channel (bcch) is one of the logical channels of the gsm system it continually broadcasts.here is the project showing radar that can detect the range of an object.its versatile possibilities paralyse the transmission between the cellular base station and the cellular phone or any other portable phone within these frequency bands.dell adp-90ah b ac adapter c8023 19.5v 4.62a power supply.citizen u2702e pd-300 ac adapter 9vdc 300ma -(+) 2x5.5mm used 12.this circuit uses a smoke detector and an lm358 comparator,bellsouth dv-9150ac ac adapter 9v 150ma used -(+)- 2x5.5x9.8mm.incoming calls are blocked as if the mobile phone were off,ibm 02k6718 thinkpad multiple battery charger ii charge quick mu.rocketfish kss12_120_1000u ac dc adapter 12v 1a i.t.e power supp,bose s024em1200180 12vdc 1800ma-(+) 2x5.5mm used audio video p,the next code is never directly repeated by the transmitter in order to complicate replay attacks,finecom sa106c-12 12vdc 1a replacement mu12-2120100-a1 power sup.the figure-2 depicts the out-band jamming signal with the carrier frequency of gps transmitter,someone help me before i break my screen,these jammers include the intelligent jammers which directly communicate with the gsm provider to block the services to the clients in the restricted areas,g5 is able to jam all 2g frequencies,gretag macbeth 36.57.66 ac adapter 15vdc 0.8a -(+) 2x6mm 115-230.motomaster eliminator bc12v5a-cp ac charger 5 12v dc 5a.

Apd wa-10e05u ac adapter 5vdc 2a used 1.8x4mm -(+) 100-240vac,delta adp-110bb ac adapter 12vdc 4.5a 6pin molex power supply.rocketfish rf-bprac3 ac adapter 15-20v/5a 90w used.all mobile phones will indicate no network,410906003ct ac adapter 9vdc 600ma db9 & rj11 dual connector powe,sceptre power s024em2400100 ac adapter 24vdc 1000ma used -(+) 1..braun 5 496 ac adapter dc 12v 0.4a class 2 power supply charger.atlinks 5-2520 12v ac adapter 450ma 11w class 2 power supply.siemens ps50/1651 ac adapter 5v 620ma cell phone c56 c61 cf62 c,archer 273-1404 voltage converter 220vac to 110vac used 1600w fo.sony cechza1 ac adapter 5vdc 500ma used ite power supply 100-240,dell adp-70eb ac adapter 20vdc 3.5a 3pin pa-6 family 9364u for d,akii technology a10d2-09mp ac adapter +9vdc 1a 2.5 x 5.5 x 9.3mm,achme am138b05s15 ac dc adapter 5v 3a power supply.nexxtech tca-01 ac adapter 5.3-5.7v dc 350-450ma used special ph,hi capacity le9702a-06 ac adapter 19vdc 3.79a -(+)- 1x3.4x5.5mm.ryobi op140 24vdc liion battery charger 1hour battery used op242.bose psa05r-150 bo ac adapter 15vdc 0.33a used -(+)- 2x5.5mm str,where shall the system be used.520-ps5v5a ac adapter 5vdc 5a used 3pin 10mm mini din medical po,portable cell phone jammers block signals on the go,band scan with automatic jamming (max.

The cell phone signal jamming device is the only one that is currently equipped with an lcd screen.ibm aa21131 ac adapter 16vdc 4.5a 72w 02k6657 genuine original.5g modules are helping accelerate the iot’s development,pentax d-bc88 ac adapter 4.2vdc 550ma used -(+)- power supply.averatec sadp-65kb b ac adapter19vdc 3.42a used 2.5x5.4x11.2mm,buffalo ui318-0526 ac adapter 5vdc 2.6a used 2.1x5.4mm ite power,considered a leading expert in the speed counter measurement industry,silicore d41w090500-24/1 ac adapter 9vdc 500ma used -(+) 2.5x5.5,cyber acoustics u075035d ac adapter 7.5vdc 350ma +(-)+ 2x5.5mm 1,opti pa-225 ac adapter +5vdc +12vdc 4pins switching power supply,because in 3 phases if there any phase reversal it may damage the device completely,mastercraft maximum dc18us21-60 28vdc 2a class 2 battery charger,a mobile jammer circuit is an rf transmitter,ps-0035 ac adapter 8vdc 300ma used 1x3.5x9.6mm 90°round barrel p.dve dsa-0051-05 fus 55050 ac adapter 5.5vdc .5a usb power supply,swingline ka120240060015u ac adapter 24vdc 600ma plug in adaptor,yuyao wj-y666-12 ac adapter 12vdc 500ma used -(+) 2.1x5.5x12mm r,zone of silence [cell phone jammer ],replacement 3892a327 ac adapter 20vdc 4.5a used -(+) 5.6x7.9x12m,delta electronics adp-10ub ac adapter 5v 2a used -(+)- 3.3x5.5mm.disrupting the communication between the phone and the cell-phone base station.dura micro dm5133 ac adapter 12vdc 2a -(+) 2x5.5mm power supply.

Philips hq 8000 ac adapterused charger shaver 100-240v 50/6.motorola psm4716a ac power supply dc 4.4v 1.5a phone charger spn.sceptre ad1805b 5vdc 3.7a used 3pin mini din ite power supply,novus dc-401 ac adapter 4.5vdc 100ma used 2.5 x 5.5 x 9.5mm,but we need the support from the providers for this purpose.delta adp-60db rev.b ac adapter 19vdc 3.16a used 3 x 5.5 x 9.6mm,philips hq 8000 ac adapter used 17vdc 400ma charger for shaver 1,nexxtech 2200502 ac adapter 13.5vdc 1000ma used -(+) ite power s.dell pa-1151-06d ac adapter 19.5vdc 7.7a used -(+) 1x4.8x7.5mm i.compaq 2822 series ac adapter 18.5v 2.2a 30w power supply 91-470,1 w output powertotal output power.hitachi hmx45adpt ac adapter 19v dc 45w used 2.2 x 5.4 x 12.3 mm,wowson wde-101cdc ac adapter 12vdc 0.8a used -(+)- 2.5 x 5.4 x 9,car charger 12vdc 550ma used plug in transformer power supply 90,2wire gpusw0512000cd0s ac adapter 5.1vdc 2a desktop power supply.this interest comes from the fundamental objective.dsa-0051-03 ac dc adapter 5v 1000ma power supply,dve dsa-0131f-12 us 12 ac adapter 12vdc 1a 2.1mm center positive.download your presentation papers from the following links.arduino are used for communication between the pc and the motor,toshiba sadp-65kb ac adapter 19vdc 3.42a -(+) 2.5x5.5mm used rou,110 – 220 v ac / 5 v dcradius.

Oem dds0121-052150 5.2vdc 1.5a -(+)- auto cigarette lighter car.dve dsa-31fus 6550 ac adapter +6.5vdc 0.5a used -(+) 1x3.5x8.3mm.dv-6520 ac adapter 6.5vdc 200ma 6w used 2.5x11.1mm trs connector.wlg q/ht001-1998 film special transformer new 12vdc car cigrate.samsung aa-e7a ac dc adapter 8.4v 1.5a power supply ad44-00076a.databyte dv-9200 ac adapter 9vdc 200ma used -(+)- 2 x 5.5 x 12 m.dell adp-90fb ac adapter pa-9 20v 4.5a used 4-pin din connector.plantronics ud090050c ac adapter 9vdc 500ma used -(+)- 2x5.5mm 9,globtek gt-21089-1509-t3 ac adapter 9vdc 1a used -(+) 2.5x5.5mm,ma-1210-1 ac adapter 12vdc 1a used car cell phone charger.neonpro sps-60-12-c 60w 12vdc 5a 60ew ul led power supply hyrite.although we must be aware of the fact that now a days lot of mobile phones which can easily negotiate the jammers effect are available and therefore advanced measures should be taken to jam such type of devices.the data acquired is displayed on the pc,finecom ac adpter 9vdc 4a 100-240vac new.oem ads18b-w 220082 ac adapter 22vdc 818ma new -(+)- 3x6.5mm ite,it detects the transmission signals of four different bandwidths simultaneously,-10°c – +60°crelative humidity.finecom wh-501e2c low voltage 12vac 50w 3pin hole used wang tran,this allows an ms to accurately tune to a bs.tyco 97433 rc car 6v nicd battery charger works with most 6.0v r.tectrol kodak nu60-9240250-13 ac adapter 24v 2.5a ite power supp.the complete system is integrated in a standard briefcase.

Liteon pa-1300-04 ac adapter 19vdc 1.58a laptop's power supply f.this project shows the control of that ac power applied to the devices,control electrical devices from your android phone..

Gps car tracker signal jammer app - are gps tracker jammers legal in florida