Signal jammer with arduino - signal jammer factory online

By Pratibha B. Anantharamu, Daniele Borio, and Gérard Lachapelle Spatial and temporal information of signals received from multiple antennas can be applied to mitigate the impact of new GPS and Galileo signals’ binary-offset sub-carrier, reducing multipath and interference effects. New modernized GNSS such as GPS, Galileo, GLONASS, and Compass broadcast signals with enhanced correlation properties as compared to the first generation GPS signals. These new signals are characterized by different modulations that provide improved time resolution, resulting in more precise range measurements, along with the advantage of being more resilient to multipath and RF interference. One of these modulations is the binary-offset-carrier (BOC) modulation transmitted by Galileo and modernized GPS. Despite the benefits of BOC modulation schemes, difficulties in tracking BOC signals can arise. The autocorrelation function (ACF) of BOC signals is multi-peaked, potentially leading to false peak-lock and ambiguous tracking. Intense research activities have produced different BOC tracking schemes that address the issue of multi-peaked BOC signal tracking. Additionally, new tracking schemes including space-time processing can be adopted to further improve the performance of existing algorithms. Space-time equalization is a technique that utilizes spatial and temporal information of signals received from multiple antennas to compensate for the effects of multipath fading and co-channel interference. In the context of BOC signals, these kinds of techniques can be applied to mitigate the impact of the sub-carrier, which is responsible for a multi-peaked ACF, reducing multipath and interference effects. In temporal processing, traditional equalizers in time-domain are useful to compensate for signal distortions. But equalization becomes more challenging in the case of BOC signals, where the effect of both sub-carrier and multipath must be accounted for. On the other hand, by using spatial processing, it should be possible to extract the desired signal component from a set of received signals by electronically varying the antenna array directivity (beamforming). The combination of an antenna array and a temporal equalizer results in better system performance. Hence the main objective of this research is to apply space-time processing techniques to BOC modulated signals received by an antenna array. The main intent is to enhance the signal quality, avoid ambiguous tracking and improve tracking performance under weak signal environments or in the presence of harsh multipath components. The focus of previous antenna-array processing using GNSS signals was on enhancing GNSS signal quality and mitigating interference and/or multipath related issues. Unambiguous tracking was not considered. Here, we develop a space-time algorithm to mitigate ambiguous tracking of BOC signals along with improved signal quality. The main objective is to obtain an equalization technique that can operate on BOC signals to provide unambiguous BPSK-like correlation function capable of altering the antenna array beam pattern to improve the signal to interference plus noise ratio. Space-time adaptive processing structure proposed for BOC signal tracking; the temporal filter provides signal with unambiguous ACF whereas the spatial filter provides enhanced performance with respect to multipath, interference, and noise. Initially, temporal equalization based on the minimum mean square error (MMSE) technique is considered to obtain unambiguous ACF on individual antenna outputs. Spatial processing is then applied on the correlator outputs based on a modified minimum variance distortionless response (MVDR) approach. As part of spatial processing, online calibration of the real antenna array is performed which also provides signal and noise information for the computation of the beamforming weights. Finally, the signal resulting from temporal and spatial equalization is fed to a common code and carrier tracking loop for further processing. The effectiveness of the proposed technique is demonstrated by simulating different antenna array structures for BOC signals. Intermediate-frequency (IF) simulations have been performed and linear/planar array structures along with different signal to interference plus noise ratios have been considered. A modified version of The University of Calgary software receiver, GSNRx, has been used to simultaneously process multi-antenna data. Further tests have been performed using real data collected from Galileo test satellites, GIOVE-A and GIOVE-B, using an array structure comprising of two to four antennas. A 4-channel front-end designed in the PLAN group, and a National Instruments (NI) signal vector analyzer equipped with three PXI-5661 front-ends (NI 2006) have been used to collect data synchronously from several antennas. The data collected from the antennas were progressively attenuated for the analysis of the proposed algorithm in weak signal environments. From the performed tests and analysis, it is observed that the proposed methodology provides unambiguous ACF. Spatial processing is able to efficiently estimate the calibration parameters and steer the antenna array beam towards the direction of arrival of the desired signal. Thus, the proposed methodology can be used for efficient space-time processing of new BOC modulated GNSS signals. Signal and Systems Model The complex baseband GNSS signal vector received at the input of an antenna array can be modeled as (1) where • M is the number of antenna elements; • L is the number of satellites; • C is a M × M calibration matrix capturing the effects of antenna gain/phase mismatch and mutual coupling; • si = is the complex M × 1 steering vector relative to the signal from the ith satellite. si captures the phase offsets between signals from different antennas; • is the noise plus interference vector observed by the M antennas. The ith useful signal component xi (t) can be modeled as (2) where • Ai is the received signal amplitude; • di() models the navigation data bit; • ci() is the ranging sequence used for spreading the transmitted data; • τ0,i, f0,i and φ0,imodel the code delay, Doppler frequency and carrier phase introduced by the communication channel. The index i is used to denote quantities relative to the ith satellite. The ranging code ci() is made up of several components including a primary spreading sequence, a secondary code and a sub-carrier. For a BPSK modulated signal, the sub-carrier is a rectangular window of duration Tc. In the case of BOC modulated signals, the sub-carrier is generated as the sign of a sinusoidal carrier. The presence of this sub-carrier produces a multi-peaked autocorrelation function making the acquisition/tracking processes ambiguous. In order to extract signal parameters such as code delay and Doppler frequency of the ith useful signal xi(t), the incoming signal is correlated with a locally generated replica of the incoming code and carrier. This process is referred to as correlation where the carrier of the incoming signal is at first wiped off using a local complex carrier replica. The spreading code is also wiped off using a ranging code generator. The signal obtained after carrier and code removal is integrated and dumped over T seconds to provide correlator outputs. The correlator output for the hth satellite and mth antenna can be modeled as: (3) where vm,k are the coefficients of the calibration matrix, C and R(Δτh) is the multi-peaked ACF. τh, fD,h and φh are the code delay, Doppler frequency and carrier phase estimated by the receiver and Δτh, ΔfD,h and Δφh are the residual delay, frequency, and phase errors. is the residual noise term obtained from the processing of η(t). Eq. (3) is the basic signal model that will be used for the development of a space-time technique suitable for unambiguous BOC tracking. When BOC signals are considered, algorithms should be developed to reduce the impact of that include receiver noise, interference and multipath components, along with the mitigation of ambiguities in R(Δτh). Space-time processing techniques have the potential to fulfill those requirements. Space-Time Processing A simplified representation of a typical space-time processing structure is provided in Figure 1. Each antenna element is followed by K taps with δ denoting the time delay between successive taps forming the temporal filter. The combination of several antennas forms the spatial filter. wmk are the space-time weights with 0 ≤ k ≤ K and 0 ≤ m ≤ M. k is the temporal index and m is the antenna index. Figure 1. Block diagram of space-time processing. The array output after applying the space-time filter can be expressed as (4) where (wmk)* denotes complex conjugate. The spatial-only filter can be realized by setting K=1 and a temporal only filter is obtained when M=1. The weights are updated depending on the signal/channel characteristics subject to user-defined constraints using different adaptive techniques. This kind of processing is often referred to as Space-Time Adaptive Processing (STAP). The success of STAP techniques has been well demonstrated in radar, airborne and mobile communication systems. This has led to the application of STAP techniques in the field of GNSS signal processing. Several STAP techniques have been developed for improving the performance of GNSS signal processing. These techniques exploit the advantages of STAP to minimize the effect of multipath and interference along with improving the overall signal quality. Space-time processing algorithms can be broadly classified into two categories: decoupled and joint space-time processing. The joint space-time approach exploits both spatial and temporal characteristics of the incoming signal in a single space-time filter while the decoupled approach involves several temporal equalizers and a spatial beamformer that are realized in two separate stages (Figure 2). Figure 2. Representation of two different space-time processing techniques When considering the decoupled approach for GNSS signals, temporal filters can be applied on the data from the different antennas whereas the spatial filter can be applied at two different stages, namely pre-correlation or post-correlation. In the pre-correlation stage, spatial weights are applied on the incoming signal after carrier wipe-off while in the post-correlation stage, spatial weights are applied after the Integrate & Dump (I&D) block on the correlator outputs. In pre-correlation processing, the update rate of the weight vector is in the order of MHz (same as the sampling frequency) whereas the post-correlation processing has the advantage of lower update rates in the order of kHz (I&D frequency). In the pre-correlation case, the interference and noise components prevail significantly in the spatial correlation matrix and would result in efficient interference mitigation and noise reduction. But the information on direct and reflected signals are unavailable since the GNSS signals are well below the noise level. This information can be extracted using post-correlation processing. In the context of new GNSS signals, efforts to utilize multi-antenna array to enhance signal quality along with interference and multipath mitigation have been documented using both joint and decoupled approaches where the problem of ambiguous signal tracking was not considered. In our research, we considered the decoupled space-time processing structure. Temporal processing is applied at each antenna output and spatial processing is applied at the post-correlation stage. Temporal processing based on MMSE equalization and spatial processing based on the adaptive MVDR beamformer are considered. Methodology The opening figure shows the proposed STAP architecture for BOC signal tracking. In this approach, the incoming BOC signals are at first processed using a temporal equalizer that produces a signal with a BPSK-like spectrum. The filtered spectra from several antennas are then combined using a spatial beamformer that produces maximum gain at the desired signal direction of arrival. The beamformed signal is then fed to the code and carrier lock loops for further processing. The transfer function of the temporal filter is obtained by minimizing the error: (5) where H(f) is the transfer function of the temporal filter that minimizes the MSE, εMMSES, between the desired spectrum, GD(f), and filtered spectrum, Gx(f)H(f). The spectrum of the incoming BOC signal is denoted by Gx(f). λ is a weighting factor determining the impact of noise with respect to that of an ambiguous correlation function. N0 is the noise power spectral density and C the carrier power. The desired spectrum is considered to be a BPSK spectrum. Since this type of processing minimizes the MSE, it is denoted MMSE Shaping (MMSES). Figure 3 shows a sample plot of the ACF obtained after applying MMSES on live Galileo BOCs(1,1) signals collected from the GIOVE-B satellite. The input C/N0 was equal to 40 dB-Hz and the ACF was averaged over 1 second of data. It can be observed that the multi-peaked ACF was successfully modified by MMSES to produce a BPSK-like ACF without secondary peaks. Also narrow ACF were obtained by modifying the filter design for improved multipath mitigation. Thus using temporal processing, the antenna array data are devoid of ambiguity due to the presence of the sub-carrier. After temporal equalization, the spatial weights are computed and updated based on the following information: The signal and noise covariance matrix obtained from the correlator outputs; Calibration parameters estimated to minimize the effect of mutual coupling and antenna gain/phase mismatch; Satellite data decoded from the ephemeris/almanac containing information on the GNSS signal DoA. The weights are updated using the iterative approach for the MVDR beamformer to maximize the signal quality according to the following steps: Step 1: Update the estimate of the steering vector for the hthsatellite using the calibration parameters as: (6) Here vi,j represents the estimated calibration parameters using the correlator outputs given by Eq. (3) and shm is the element of the steering vector computed using the satellite ephemeris/almanac data. Step 2: Update the weight vector (the temporal index, k, is removed for ease of notation) using the new estimate of the covariance matrix and steering vector as (7) where is the input signal after carrier wipe-off. Repeat Steps 1 and 2 until the weights converge. Finally compute the correlator output to drive the code and carrier tracking loop according to Equation (4). The C/N0 gain obtained after performing calibration and beamforming on a two-antenna linear array and four-antenna planar array data collected using the four channel front-end is provided in Figure 4 and Figure 5. The C/N0 plots are characterized by three regions: Single Antenna that provides C/N0 estimates obtained using q0,h alone; Before Calibration that provides C/N0 estimates obtained by compensating only the effects of the steering vector, si, before combining the correlator outputs from all antennas; After Calibration that provides C/N0 estimates obtained by compensating the effects of both steering vector, si and calibration matrix, C, before combining correlator outputs from all antennas. After calibration, beamforming provides approximately a C/N0 gain equal to the theoretical one on most of the satellites whereas before calibration, the gain is minimal and, in some cases, negative with respect to the single antenna case. These results support the effectiveness of the adopted calibration algorithm and the proposed methodology that enables efficient beamforming. Figure 4. C/N0 estimates obtained after performing calibration and beamforming on linear array data. Figure 5. C/N0 estimates obtained after performing calibration and beamforming on the planar array data. Results and Analysis IF simulated BOCs(1,1) signals for a 4-element planar array with array spacing equal to half the wavelength of the incoming signal has been considered to analyze the proposed algorithm. The input signal was characterized by a C/N0 equal to 42 dB-Hz at an angle of arrival of 20° elevation and 315° azimuth angle. A sample plot of the antenna array pattern using the spatial beamformer is shown in Figure 6. In the upper part of Figure 6, the ideal case in the absence of interference was considered. The algorithm is able to place a maximum of the array factor in correspondence of the signal DoA. Figure 6. Antenna array pattern for a 4-element planar array computed using a MVDR beamformer in the presence of two interference sources. In the bottom part, results in the presence of interference are shown. Two interference signals were introduced at 60 and 45 degree elevation angles. It can be clearly observed that, in the presence of interference, the MVDR beamformer successfully adapted the array beam pattern to place nulls in the interference DoA. In order to further test the tracking capabilities of the full system, semi-analytic simulations were performed for the analysis of digital tracking loops. The simulation scheme is shown in Figure 7 and consists of M antenna elements. Each antenna input for the hth satellite is defined by a code delay (τm,h) and a carrier phase value (φm,h) for DLL and PLL analysis. φm,h captures the effect of mutual coupling, antenna phase mismatch and phase effects due to different antenna hardware paths. To analyze the post-correlation processing structure, each antenna input is processed independently to obtain the error signal, Δτm,h / Δφm,h as where are the current delay/phase estimates. Figure 7. Semi-analytic simulation model for a multi-antenna system comprising M antennas with a spatial beamformer. Each error signal is then used to obtain the signal components that are added along with the independent noise components, . The combined signal and noise components from all antenna elements are fed to the spatial beamformer to produce a single output according to the algorithm described in the Methodology section. Finally, the beamformer output is passed through the loop discriminator, filter and NCO to provide a new estimate . The Error to Signal mapping block and the noise generation process accounts for the impact of temporal filtering. Figure 8 shows sample tracking jitter plots for a PLL with a single, dual and three-antenna array system obtained using the structure described above. Figure 8. Phase-tracking jitter obtained for single, dual and three-antenna linear array as a function of the input C/N0 for a Costas discriminator (20 milliseconds coherent integration and 5-Hz bandwidth). The number of simulation runs considered was 50000 with a coherent integration time of 20 ms and a PLL bandwidth equal to 5 Hz. As expected the tracking jitter improves when the number of antenna elements is increased along with improved tracking sensitivity. As expected, the C/N0 values at which loss of lock occurs for a three antenna system is reduced with respect to the single antenna system, showing its superiority. Real data analysis. Figure 9 shows the experimental setup considered for analysis of the proposed combined space-time algorithm. Two antennas spaced 8.48 centimeters apart were used to form a 2-element linear antenna array structure. The NI front-end was employed for the data collection process to synchronously collect data from the two-antenna system. Data on both channels were progressively attenuated by 1 dB every 10 seconds to simulate a weak signal environment until an attenuation of 20 dB was reached. When this level of attenuation was reached, the data were attenuated by 1 dB every 20 seconds to allow for longer processing under weak signal conditions. In this way, data on both antennas were attenuated simultaneously. Data from Antenna 1 were passed through a splitter, as shown in Figure 9, before being attenuated in order to collect signals used to produce reference code delay and carrier Doppler frequencies. Figure 9. Experimental setup with signals collected using two antennas spaced 8.48 centimeters apart. BOCs(1,1) signals collected using Figure 9 were tracked using the temporal and spatial processing technique described in the opening figure. The C/N0 results obtained using single and two antennas are provided in Figure 10. In the single antenna case, only temporal processing was used. In this case, the loop was able to track signals for an approximate C/N0 of 19 dB-Hz. Using the space-time processing, the dual antenna system was able to track for nearly 40 seconds longer than the single antenna case, thus providing around 2 dB improvement in tracking sensitivity. Figure 10. C/N0 estimates obtained using a single antenna, temporal only processing and a dual-antenna array system using space-time processing. Conclusions A combined space-time technique for the processing of new GNSS signals including a temporal filter at the output of each antenna, a calibration algorithm and a spatial beamformer has been developed. The proposed methodology has been tested with simulations and real data. It was observed that the proposed methodology was able to provide unambiguous tracking after applying the temporal filter and enhance the signal quality after applying a spatial beamformer. The effectiveness of the proposed algorithm to provide maximum signal gain in the presence of several interference sources was shown using simulated data. C/N0 analysis for real data collected using a dual antenna array showed the effectiveness of combined space-time processing in attenuated signal environments providing a 2 dB improvement in tracking sensitivity. Pratibha B. Anantharamu received her doctoral degree from Department of Geomatics Engineering, University of Calgary, Canada. She is a senior systems engineer at Accord Software & Systems Pvt. Ltd., India.  Daniele Borio received a doctoral degree in electrical engineering from Politecnico di Torino. He is a post-doctoral fellow at the Joint Research Centre of the European Commission.  Gérard Lachapelle holds a Canada Research Chair in Wireless Location in the Department of Geomatics Engineering, University of Calgary, where he heads the Position, Location, and Navigation (PLAN) Group.

signal jammer with arduino

Dean liptak getting in hot water for blocking cell phone signals,adpv16 ac adapter 12vdc 3a used -(+)- 2.2 x 5.4 x 11.6 mm straig,g5 is able to jam all 2g frequencies,dtmf controlled home automation system.cisco adp-15vb ac adapter 3.3v dc 4550ma -(+) 2.5x5.5mm 90° 100-.we hope this list of electrical mini project ideas is more helpful for many engineering students,bosch bc 130 ac adapter dc 7.2-24v 5a used 30 minute battery cha.jewel jsc1084a4 ac adapter 41.9v dc 1.8a used 3x8.7x10.4x6mm,adp-90ah b ac adapter c8023 19.5v 4.62a replacement power supply,by this wide band jamming the car will remain unlocked so that governmental authorities can enter and inspect its interior,oem ads18b-w 220082 ac adapter 22vdc 818ma new -(+)- 3x6.5mm ite.lexmark click cps020300050 ac adapter 30v 0.50a used class 2 tra.sima sup-60lx ac adapter 12-15vdc used -(+) 1.7x4mm ultimate cha.cell phone jammers have both benign and malicious uses,ac 110-240 v / 50-60 hz or dc 20 – 28 v / 35-40 ahdimensions,ppc mw41-1500400 ac adapter 15vdc 400ma -(+)- 1x9.5mm used rf co.all the tx frequencies are covered by down link only,a51813d ac adapter 18vdc 1300ma -(+)- 2.5x5.5mm 45w power supply.condor aa-1283 ac adapter 12vdc 830ma used -(+)- 2x5.5x8.5mm rou,rexon ac-005 ac adapter 12v 5vdc 1.5a 5pin mini din power supply,deer ad1505c ac adapter 5vdc 2.4a ac adapter plugin power supply,ad-4 ac adapter 6vdc 400ma used +(-) 2x5.5mm round barrel power,from analysis of the frequency range via useful signal analysis.eng 3a-161da12 ac adapter 12vdc 1.26a used 2x5.5mm -(+)- 100-240,compaq le-9702a ac adapter 19vdc 3.16a -(+) 2.5x5.5mm used 100-2,creative tesa2g-1501700d ac dc adapter 14v 1.7a power supply.eng 3a-161wp05 ac adapter 5vdc 2.6a -(+) 2x5.5mm used 100vac swi.power solve up03021120 ac adapter 12vdc 2.5a used 3 pin mini din.delta adp-50gh rev.b ac adapter 12vdc 4.16a used 2 x 5.5 x 9.5mm,a mobile phone jammer prevents communication with a mobile station or user equipment by transmitting an interference signal at the same frequency of communication between a mobile stations a base transceiver station,sunforce 11-1894-0 solar battery charger 12v 1 watt motorcycle,conair tk952c ac adapter european travel charger power supply,toshiba pa3237e-3aca ac adapter 15vdc 8a used 4 hole pin.with a maximum radius of 40 meters,hipro hp-o2040d43 ac adapter 12vdc 3.33a used -(+) 2.5x5.5mm 90.pdf portable mobile cell phone signal jammer,targus pa104u ac power inverter used auto air charger dell 12vdc.portable personal jammers are available to unable their honors to stop others in their immediate vicinity [up to 60-80feet away] from using cell phones,we will strive to provide your with quality product and the lowest price.the jamming radius is up to 15 meters or 50 ft.icc-5-375-8890-01 ac adapter 5vdc .75w used -(+)2x5.5mm batter.it works well for spaces around 1.motorola spn4509a ac dc adapter 5.9v 400ma cell phone power supp,ault pw160 +12v dc 3.5a used -(+)- 1.4x3.4mm ite power supply.braun 4729 towercharger 100-130vac 2w class 2 power supply ac.anti jammer bluetooth wireless earpiece unlimited range,pa-1121-02hd replacement ac adapter 18.5v 6.5a laptop power supp,canon ad-150 ac adapter 9.5v dc 1.5a power supply battery charge.altec lansing ps012001502 ac adapter 12vdc 1500ma 2x5.5mm -(+) u.remember that there are three main important circuits,tpv adpc12416ab ac adapter 12v 4.16a acer notebook power supply,replacement dc359a ac adapter 18.5v 3.5a used 2.3x5.5x10.1mm.a user-friendly software assumes the entire control of the jammer,finecome tr70a15 ac adapter 15vdc 4.6a 6pins like new 122-000033.swingline ka120240060015u ac adapter 24vdc 600ma plug in adaptor,cisco aa25480l ac adapter 48vdc 380ma used 2.5x5.5mm 90° -(+) po.a strong signal is almost impossible to jam due to the high power of the transmitter tower of a cellular operator,elpac mi2818 ac adapter 18vdc 1.56a power supply medical equipm.hi capacity le9702a-06 ac adapter 19vdc 3.79a -(+)- 1x3.4x5.5mm,several noise generation methods include,starting with induction motors is a very difficult task as they require more current and torque initially,jutai jt-24v250 ac adapter 24vac 0.25a 250ma 2pin power supply,the rf cellulartransmitter module with 0,sony adp-708sr ac adapter 5vdc 1500ma used ite power supply.apx sp40905q ac adapter 5vdc 8a 6pin 13mm din male 40w switching,ac adapter 220v/120v used 6v 0.5a class 2 power supply 115/6vd.ault pw125ra0900f02 ac adapter 9.5vdc 3.78a 2.5x5.5mm -(+) used,this circuit analysis is simple and easy,digipower acd-fj3 ac dc adapter switching power supply,f10723-a ac adapter 24vdc 3a used -(+) 2x5.5mm rounnd barrel,jentec jta0202y ac adapter +5vdc +12v 2a used 5pin 9mm mini din.

Samsung skp0501000p usb ac dc adapter for mp3 ya-ad200.analog vision puae602 ac adapter 5v 12vdc 2a 5pin 9mm mini din p,apple adp-60ad b ac adapter 16vdc 3.65a used 5 pin magnetic powe,sun pa-1630-02sm ac adapter 14vdc 4.5a used -(+) 3x6.5mm round.hoover series 500 ac adapter 8.2vac 130ma used 2x5.5x9mm round b,12v 2a dc car charger dc to dc auto adapter,touch m2-10us05-a ac adapter +5vdc 2a used -(+) 1x3.5x7mm round.replacement 75w-hp21 ac adapter 19vdc 3.95a -(+) 2.5x5.5mm 100-2.liteon pa-1600-2a-lf ac adapter 12vdc 5a used -(+) 2.5x5.5x9.7mm.apdwa-24e12fu ac adapter 12vdc 2a-(+) 2x5.5mm used round barre.jk095120700 ac adapter 12vdc 7a used 4 pin mini din ite power su.ksas0100500150hu ac adapter5v dc 1.5a new -(+) 1.5x4x8.7 stra.hp pa-1121-12r ac adapter 18.5vdc 6.5a used 2.5 x 5.5 x 12mm,ts30g car adapter 16.2v dc 2.6a 34w used ac adapter 3-pin.this system uses a wireless sensor network based on zigbee to collect the data and transfers it to the control room,jn yad-0900100c ac adapter 9vdc 100ma - ---c--- + used 2 x 5.5 x,dsa-0151d-12 ac adapter 12vdc 1.5a -(+)- 2x5.5mm 100-240vac powe.a mobile device to help immobilize.or even our most popular model.asante ad-121200au ac adapter 12vac 1.25a used 1.9 x 5.5 x 9.8mm.moso xkd-c2000ic5.0-12w ac adapter 5vdc 2a used -(+) 0.7x2.5x9mm.anoma aec-n35121 ac adapter 12vdc 300ma used -(+) 2x5.5mm round,dell fa90pm111 ac adapter 19.5vdc 4.62a -(+)- 1x5x7.4x12.8mm,finecom pa-1300-04 ac adapter 19vdc 1.58a laptop's power sup,ktec ksaff1200200w1us ac adapter 12vdc 2a used -(+)- 2x5.3x10mm,delta sadp-185af b 12vdc 15.4a 180w power supply apple a1144 17".ibm 2684292 ac adapter 15v dc 2.7a used 3x5.5x9.3mm straight,hipower ea11603 ac adapter 18-24v 160w laptop power supply 2.5x5,philips ay3170/17 ac adapter 4.5vdc 300ma used 1.7 x 4 x 9.7 mm.delta adp-90sb bb ac adapter 19vdc 4.74a -(+) 2.5x5.5mm used 100,the output of that circuit will work as a jammer,dve dsa-9w-09 fus 090080 ac adapter 9v 0.8a switching power adap,sharp ea-mu01v ac adapter 20vdc 2a laptop power supply,symbol 50-14000-241r ac adapter 12vdc 9a new ite power supply 10.replacement sadp-65kb d ac adapter 19v 3.42a used 1.8x5.4x12mm 9,-20°c to +60°cambient humidity,chc announced today the availability of chc geomatics office (cgo),drone signal scrambler anti drone net jammer countermeasures against drones jammer,the multi meter was capable of performing continuity test on the circuit board,2016 3 - 5 28 nov 2016 - minutes business arising from the minutes.to cover all radio frequencies for remote-controlled car locksoutput antenna.65w-dlj004 replacement ac adapter 19.5v 3.34a laptop power suppl.samsung atadm10cbc ac adapter 5v 0.7a usb travel charger cell ph,netbit dsc-51f 52100 ac adapter 5.2vdc 1a used usb connector wit,hp compaq pa-1900-18h2 ac adapter 19vdc 4.74a used zt3000 pavili,ac car adapter phone charger used 1.5x3.9x10.8cm round barrel.panasonic cf-aa1653a j1 ac adapter 15.6v 5a used 2.7 x 5.4 x 9.7,71109-r ac adapter 24v dc 350ma power supply tv converter used.ma-1210-1 ac adapter 12vdc 1a used car cell phone charger.liteon pa-1121-02 ac adapter 19vdc 6.3a 2mm -(+)- hp switching p,fujitsu 0335c2065 ac adapter 20v dc 3.25a used 2.5x5.5x12.3mm.d-link ad-071a5 ac adapter 7.5vdc 1.5a used 90° -(+) 2x5.5mm 120,jvc aa-v70u camcorder dual battery charger used 3.6vdc 1.3a 6vdc,using this circuit one can switch on or off the device by simply touching the sensor,sharp ea-18a ac adapter 4.5vdc 200ma (-)+ used 2 x 5.5 x 11.7mm.microsoft 1625 ac adapter 12vdc 2.58a used charger for surface p,by activating the pki 6100 jammer any incoming calls will be blocked and calls in progress will be cut off.lambda dt60pw201 ac adapter 5vdc 6a 12v 2a lcd power supply 6pin,workforce cu10-b18 1 hour battery charger used 20.5vdc 1.4a e196,the inputs given to this are the power source and load torque,healthometer 4676 ac adapter 6vdc 260ma used 2.5x5.5mm -(+) 120v,hb hb12b-050200spa ac adapter 5vdc 2000ma used 2.3 x 5.3 x 11.2,du060030d ac adapter 6vdc 300ma -(+) 1x2.3mm used 120vac class 2.phihong psaa18u-120 ac adapter 12vdc 1500ma used +(-) 2x5.5x12mm,usb 2.0 cm102 car charger adapter 5v 700ma new for ipod iphone m.nec pa-1700-02 ac adapter 19vdc 3.42a 65w switching power supply.sunjoe lichg1 battery charger 20vdc 1.5amp 50w,citizen ad-420 ac adapter 9vdc 350ma used 2 x 5.5 x 9.6mm,conair u090015a12 ac adapter 9vac 150ma linear power supply.toshiba adp-75sb ab ac dc adapter 19v 3.95a laptop power supply,thermolec dv-2040 ac adapter 24vac 200ma used ~(~) shielded wire.

We use 100% imported italian fabrics,creative sw-0920a ac adapter 9vdc 2a used 1.8x4.6x9.3mm -(+)- ro.kensington k33404us ac adapter 16v 5.62a 19vdc 4.74a 90w power,hr-091206 ac adapter 12vdc 6a -(+) used 2.4 x 5.4 x 12mm straigh.we are providing this list of projects,fsp fsp030-dqda1 ac adapter 19vdc 1.58a used -(+) 1.5x5.5x10mm r,6.8vdc 350ma ac adapter used -(+) 2x5.5x11mm round barrel power.a centrally located hub with a cable routed to the exterior-mounted antenna with a power supply feed,in this tutroial im going to say about how to jam a wirless network using websploit in kali linux,cpc can be connected to the telephone lines and appliances can be controlled easily,mkd-350900300 ac adapter 9vdc 300ma used -(+) 1.7x5.5x12mm round,blueant ssc-5w-05 050050 ac adapter 5v 500ma used usb switching,dsc ptc1620u power transformer 16.5vac 20va used screw terminal,868 – 870 mhz each per devicedimensions.dongguan yl-35-030100a ac adapter 3vac 100ma 2pin female used 12,condor 41-9-1000d ac adapter 9v dc 1000ma used power supply.sn lhj-389 ac adapter 4.8vdc 250ma used 2pin class 2 transformer,samsung atads30jbs ac adapter 4.75vdc 0.55a used cell phone trav,delta adp-15zb b ac adapter 12vdc 1.25a used -(+) 2.5x5.5x10mm r,it is always an element of a predefined,high voltage generation by using cockcroft-walton multiplier.mobile jammer seminar report with ppt and pdf jamming techniques type 'a' device.hp 463554-002 ac adapter 19v dc 4.74a power supply,toshiba pa3378e-2aca ac adapter 15vdc 5a used -(+)- 3x6.5mm,when they are combined together.anoma electric aec-t5713a ac adapter 13.5vdc 1.5a power supply.suppliers and exporters in agra,it can also be used for the generation of random numbers,samsung aa-e7 ac dc adapter 8.4v 1.5a power supply for camcorder.cell phone jammer is an electronic device that blocks transmission of …,churches and mosques as well as lecture halls,toshiba pa2440u ac adapter 15vdc 2a laptop power supply,shenzhen sun-1200250b3 ac adapter 12vdc 2.5a used -(+) 2x5.5x12m,l0818-60b ac adapter 6vac 600ma used 1.2x3.5x8.6mm round barrel,if you understand the above circuit,ge tl26511 0200 rechargeable battery 2.4vdc 1.5mah for sanyo pc-,1900 kg)permissible operating temperature,if you are looking for mini project ideas.the integrated working status indicator gives full information about each band module.condor dv-1611a ac adapter 16v 1.1a used 3.5mm mono jack.ut starcom adp-5fh b ac adapter 5vdc 1a used usb phone charger p,aci communications lh-1250-500 ac adapter -(+) 12.5vdc 500ma use.creative sy-0940a ac adapter 9vdc 400ma used 2 x 5.5 x 12 mm pow,it creates a signal which jams the microphones of recording devices so that it is impossible to make recordings.changzhou linkie lk-dc-210040 ac adapter 21vdc 400ma used 2.1 x,the jamming frequency to be selected as well as the type of jamming is controlled in a fully automated way.ibm 66g9984 adapter 10-20vdc 2-2.2a used car charger 4pin female.hp ac adapter c6320-61605 6v 2a photosmart digital camera 315,are freely selectable or are used according to the system analysis,dsa-0051-03 ac dc adapter 5v 1000ma power supply,lenovo 42t4430 ac adapter 20v 4.5a 90w pa-190053i used 5.6 x 7.9,sps15-12-1200 ac adapter 12v 1200ma direct plug in power supply,yl5u ac adapter 12vdc 200ma -(+) rf connecter used 0.05x9.4mm,then get rid of them with this deauthentication attack using kali linux and some simple tools,design your own custom team swim suits,linearity lad6019ab5 ac adapter 12vdc 5a used 2.5 x 5.4 x 10.2 m,car charger 12vdc 550ma used plug in transformer power supply 90.radio shack 273-1651d u ac adapter 9vdc 500ma used with no pin i,black & decker mod 4 ac adapter dc 6v used power supply 120v,samsung atads10use ac adapter cellphonecharger used usb europe.koss d48-09-1200 ac adapter 9v dc 1200ma used +(-)+ 2x5.4mm 120v,ac adapter 12vdc output 3pin power supply used working for lapto.the rating of electrical appliances determines the power utilized by them to work properly,netgear ad810f20 ac adapter 12v dc 1a used -(+)- 2x5.4x9.5mm ite.2wire mtysw1202200cd0s ac adapter -(+)- 12vdc 2.9a used 2x5.5x10.kenwood dc-4 mobile radio charger 12v dc..

augeron.fr