Autonomous GPS Positioning at High Earth Orbits
To initially acquire the GPS signals, a receiver also would have to search quickly through the much larger range of possible Doppler shifts and code delays than those experienced by a terrestrial receiver.
By William Bamford, Luke Winternitz and Curtis Hay
INNOVATION INSIGHTS by Richard Langley
GPS RECEIVERS have been used in space to position and navigate satellites and rockets for more than 20 years. They have also been used to supply accurate time to satellite payloads, to determine the attitude of satellites, and to profile the Earth’s atmosphere. And GPS can be used to position groups of satellites flying in formation to provide high-resolution ground images as well as small-scale spatial variations in atmospheric properties and gravity.
Receivers in low Earth orbit have virtually the same view of the GPS satellite constellation as receivers on the ground. But satellites orbiting at geostationary altitudes and higher have a severely limited view of the main beams of the GPS satellites. The main beams are either directed away from these high-altitude satellites or they are blocked to a large extent by the Earth.
Typically, not even four satellites can be seen by a conventional receiver. However, by using the much weaker signals emitted by the GPS satellite antenna side lobes, a receiver may be able track a sufficient number of satellites to position and navigate itself. To initially acquire the GPS signals, a receiver also would have to search quickly through the much larger range of possible Doppler shifts and code delays than those experienced by a terrestrial receiver.
In this month’s column, William Bamford, Luke Winternitz, and Curtis Hay discuss the architecture of a receiver with these needed capabilities — a receiver specially designed to function in high Earth orbit. They also describe a series of tests performed with a GPS signal simulator to validate the performance of the receiver here on the ground — well before it debuts in orbit.
“Innovation” is a regular column featuring discussions about recent advances in GPS technology and its applications as well as the fundamentals of GPS positioning. The column is coordinated by Richard Langley of the Department of Geodesy and Geomatics Engineering at the University of New Brunswick, who appreciates receiving your comments and topic suggestions. To contact him, see the “Columnists” section in this issue.
Calculating a spacecraft’s precise location at high orbits — 22,000 miles (35,400 kilometers) and beyond — is an important and challenging problem. New and exciting opportunities become possible if satellites are able to autonomously determine their own orbits.
First, the repetitive task of periodically collecting range measurements from terrestrial antennas to high-altitude spacecraft becomes less important — this lessens competition for control facilities and saves money by reducing operational costs. Also, autonomous navigation at high orbital altitudes introduces the possibility of autonomous station-keeping. For example, if a geostationary satellite begins to drift outside of its designated slot, it can make orbit adjustments without requiring commands from the ground. Finally, precise onboard orbit determination opens the door to satellites flying in formation — an emerging concept for many scientific space applications.
Realizing these benefits is not a trivial task. While the navigation signals broadcast by GPS satellites are well suited for orbit and attitude determination at lower altitudes, acquiring and using these signals at geostationary (GEO) and highly elliptical orbits (HEOs) is much more difficult. This situation is illustrated in FIGURE 1.
Figure 1. GPS signal reception at GEO and HEO orbital altitudes.
The light blue trace shows the GPS orbit at approximately 12,550 miles (20,200 kilometers) altitude. GPS satellites were designed to provide navigation signals to terrestrial users — because of this, the antenna array points directly toward the Earth. GEO and HEO orbits, however, are well above the operational GPS constellation, making signal reception at these altitudes more challenging. The nominal beamwidth of a Block II/IIA GPS satellite antenna array is approximately 42.6 degrees. At GEO and HEO altitudes, the Earth blocks most of these primary beam transmissions, leaving only a narrow region of nominal signal visibility near the limb of the Earth.This region is highlighted in gray.
If GPS receivers at GEO and HEO orbits were designed to use these higher power signals only, precise orbit determination would not be practical. Fortunately, the GPS satellite antenna array also produces side-lobe signals at much lower power levels. The National Aeronautics and Space Administration (NASA) has designed and tested the Navigator, a new GPS receiver that can acquire and track these weaker signals, dramatically increasing signal visibility at these altitudes.
While using much weaker signals is a fundamental requirement for a high orbital altitude GPS receiver, it is certainly not the only challenge. Other unique characteristics of this application must also be considered. For example, position dilution of precision (PDOP) figures are much higher at GEO and HEO altitudes because visible GPS satellites are concentrated in a much smaller region with respect to the spacecraft antenna. These poor PDOP values contribute considerable error to the point-position solutions calculated by the spacecraft GPS receiver.
Extreme Conditions. Finally, spacecraft GPS receivers must be designed to withstand a variety of extreme environmental conditions. Variations in acceleration between launch and booster separation are extreme. Temperature gradients in the space environment are also severe. Furthermore, radiation effects are a major concern — spaceborne GPS receivers should be designed with radiation-hardened parts to minimize damage caused by continuous exposure to low-energy radiation as well as damage and operational upsets from high-energy particles. Perhaps most importantly, we typically cannot repair or modify a spaceborne GPS receiver after launch. Great care must be taken to ensure all performance characteristics are analyzed before liftoff.
Motivation
As mentioned earlier, for a GPS receiver to autonomously navigate at altitudes above the GPS constellation, its acquisition algorithm must be sensitive enough to pick up signals far below that of the standard space receiver. This concept is illustrated in FIGURE 2. The colored traces represent individual GPS satellite signals. The topmost dotted line represents the typical threshold of traditional receivers. It is evident that such a receiver would only be able to track a couple of the strong, main-lobe signals at any given time, and would have outages that can span several hours.
The lower dashed line represents the design sensitivity of the Navigator receiver. The 10 dB reduction allows Navigator to acquire and track the much weaker side-lobe signals. These side lobes augment the main lobes when available, and almost completely eliminate any GPS signal outages. This improved sensitivity is made possible by the specialized acquisition engine built into Navigator’s hardware.
Figure 2. Simulated received power at GEO orbital altitude.
Acquisition Engine
Signal acquisition is the first, and possibly most difficult, step in the GPS signal processing procedure. The acquisition task requires a search across a three-dimensional parameter space that spans the unknown time delay, Doppler shift, and the GPS satellite pseudorandom noise codes. In space applications, this search space can be extremely large, unless knowledge of the receiver’s position, velocity, current time, and the location of the desired GPS satellite are available beforehand.
Serial Search. The standard approach to this problem is to partition the unknown Doppler-delay space into a sufficiently fine grid and perform a brute force search over all possible grid points. Traditional receivers use a handful of tracking correlators to serially perform this search. Without sufficient information up front, this process can take 10–20 minutes in a low Earth orbit (LEO), or even terrestrial applications, and much longer in high-altitude space applications. This delay is due to the exceptionally large search space the receiver must hunt through and the inefficiency of serial search techniques.
Acquisition speed is relevant to the weak signal GPS problem, because acquiring weak signals requires the processing of long data records. As it turns out, using serial search methods (without prior knowledge) for weak signal acquisition results in prohibitively long acquisition times.
Many newer receivers have added specialized fast-acquisition capability. Some employ a large array of parallel correlators; others use a 32- to 128-point fast Fourier transform (FFT) method to efficiently resolve the frequency dimension. These methods can significantly reduce acquisition time. Another use of the FFT in GPS acquisition can be seen in FFT-correlator-based block-processing methods, which offer dramatically increased acquisition performance by searching the entire time-delay dimension at once. These methods are popular in software receivers, but because of their complexity, are not generally used in hardware receivers.
Exceptional Navigator. One exception is the Navigator receiver. It uses a highly specialized hardware acquisition engine designed around an FFT correlator. This engine can be thought of as more than 300,000 correlators working in parallel to search the entire Doppler-delay space for any given satellite. The module operates in two distinct modes: strong signal mode and weak signal mode. Strong signal mode processes a 1 millisecond data record and can acquire all signals above –160 dBW in just a few seconds. Weak signal mode has the ability to process arbitrarily long data records to acquire signals down to and below –175 dBW. At this level, 0.3 seconds of data are sufficient to reliably acquire a signal.
Additionally, because the strong, main-lobe, signals do not require the same sensitivity as the side-lobe signals, Navigator can vary the length of the data records, adjusting its sensitivity on the fly. Using essentially standard phase-lock-loop/delay-lock-loop tracking methods, Navigator is able to track signals down to approximately –175 dBW. When this tracking loop is combined with the acquisition engine, the result is the desired 10 dB sensitivity improvement over traditional receivers. FIGURE 3 illustrates Navigator’s acquisition engine.
Powered by this design, Navigator is able to rapidly acquire all GPS satellites in view, even with no prior information. In low Earth orbit, Navigator typically acquires all in-view satellites within one second, and has a position solution as soon as it has finished decoding the ephemeris from the incoming signal. In a GEO orbit, acquisition time is still typically under a minute.
Figure 3. Navigator signal acquisition engine.
Navigator breadboard.
GPS constellation simulator.
Navigator Hardware
Outside this unique acquisition module, Navigator employs the traditional receiver architecture: a bank of hardware tracking correlators attached to an embedded microprocessor. Navigator’s GPS signal-processing hardware, including both the tracking correlators and the acquisition module, is implemented in radiation-hardened field programmable gate arrays (FPGAs). The use of FPGAs, rather than an application-specific integrated circuit, allows for rapid customization for the unique requirements of upcoming missions. For example, when the L2 civil signal is implemented in Navigator, it will only require an FPGA code change, not a board redesign.
The current Navigator breadboard—which, during operation, is mounted to a NASA-developed CPU card—is shown in the accompanying photo. The flight version employs a single card design and, as of the writing of this article, is in the board-layout phase. Flight-ready cards will be delivered in October 2006.
Integrated Navigation Filter
Even with its acquisition engine and increased sensitivity, Navigator isn’t always able to acquire the four satellites needed for a point solution at GEO altitudes and above. To overcome this, the GPS Enhanced Onboard Navigation System (GEONS) has been integrated into the receiver software. GEONS is a powerful extended Kalman filter with a small package size, ideal for flight-software integration. This filter makes use of its internal orbital dynamics model in conjunction with incoming measurements to generate a smooth solution, even if fewer than four GPS satellites are in view.
The GEONS filter combines its high-fidelity orbital dynamics model with the incoming measurements to produce a smoother solution than the standard GPS point solution. Also, GEONS is able to generate state estimates with any number of visible satellites, and can provide state estimation even during complete GPS coverage outages.
Hardware Test Setup
We used an external, high-fidelity orbit propagator to generate a two-day GEO trajectory, which we then used as input for the Spirent STR4760 GPS simulator. This equipment, shown in the accompanying photo, combines the receiver’s true state with its current knowledge of the simulated GPS constellation to generate the appropriate radio frequency (RF) signals as they would appear to the receiver’s antenna. Since there is no physical antenna, the Spirent SimGEN software package provides the capability to model one.
The Navigator receiver begins from a cold start, with no advance knowledge of its position, the position of the GPS satellites, or the current time. Despite this lack of information, Navigator typically acquires its first satellites within a minute, and often has its first position solution within a few minutes, depending on the number of GPS satellites in view. Once a position solution has been generated, the receiver initializes the GEONS navigation filter and provides it with measurements on a regular, user-defined basis. The Navigator point solution is output through a high-speed data acquisition card, and the GEONS state estimates, covariance, and measurement residuals are exported through a serial connection for use in data analysis and post-processing.
We configured the GPS simulator to model the receiving antenna as a hemispherical antenna with a 135-degree field-of-view and 4 dB of received gain, though this antenna would not be optimal for the GEO case. Assuming a nadir-pointing antenna, all GPS signals are received within a 40-degree angle with respect to the bore sight. Furthermore, no signals arrive from between 0 and 23 degrees elevation angle because the Earth obstructs this range. An optimal GEO antenna (possibly a high-gain array) would push all of the gain into the feasible elevation angles for signal reception, which would greatly improve signal visibility for Navigator (a traditional receiver would still not see the side lobes). Nonetheless, the following results provide an important baseline and demonstrate that a high-gain antenna, which would increase size and cost of the receiver, may not be necessary with Navigator. The GPS satellite transmitter gain patterns were set to model the Block II/IIA L1 reference gain pattern.
Simulation Results
To validate the receiver designs, we ran several tests using the configuration described above. The following section describes the results from a subset of these tests.
Tracked Satellites. The top plot of FIGURE 4 illustrates the total number of satellites tracked by the Navigator receiver during a two-day run with the hemispherical antenna. On average, Navigator tracked between three and four satellites over the simulation period, but at times as many as six and as few as zero were tracked. The middle pane depicts the number of weak signals tracked—signals with received carrier-to-noise-density ratio of 30 dB-Hz or less. The bottom panel shows how many satellites a typical space receiver would pick up. It is evident that Navigator can track two to three times as many satellites at GEO as a typical receiver, but that most of these signals are weak.
Figure 4. Number of satellites tracked in GEO simulation.
Acquisition Thresholds. The received power of the signals tracked with the hemispherical antenna is plotted in the top half of FIGURE 5. The lowest power level recorded was approximately –178 dBW, 3 dBW below the design goal. (Note the difference in scale from Figure 1, which assumed an additional 6 dB of antenna gain.) The bottom half of Figure 5 shows a histogram of the tracked signals. It is clear that most of the signals tracked by Navigator had received power levels around –175 dBW, or 10 dBW weaker than a traditional receiver’s acquisition threshold.
Figure 5. Signal tracking data from GEO simulation.
Navigation Filter. To validate the integration of the GEONS software, we compared its estimated states to the true states over the two-day period. These results are plotted in FIGURE 6. For this simulation, we assumed that GPS satellite clock and ephemeris errors could be corrected by applying NASA’s Global Differential GPS System corrections, and errors caused by the ionosphere could be removed by masking signals that passed close to the Earth’s limb. The truth environment consisted of a 70X70 degree-and-order gravity model and sun-and-moon gravitational effects, as well as drag and solar-radiation pressure forces. GEONS internally modeled a 10X10 gravity field, solar and lunar gravitational forces, and estimated corrections to drag and solar-radiation pressure parameters. (Note that drag is not a significant error source at these altitudes.) Though the receiver produces pseudorange, carrier-phase, and Doppler measurements, only the pseudorange measurement is being processed in GEONS.
Figure 6. GEONS state estimation errors for GEO simulation.
The results, compiled in TABLE 1, show that the 3D root mean square (r.m.s.) of the position error was less than 10 meters after the filter converges. The velocity estimation agreed very well with the truth, exhibiting less than 1 millimeter per second of three-dimensional error. Navigator can provide excellent GPS navigation data at low Earth orbit as well, with the added benefit of near instantaneous cold-start signal acquisition. For completeness, the low Earth orbit results are included in Table 1.
Navigator’s Future
Navigator’s unique features have attracted the attention of several NASA projects. In 2007, Navigator is scheduled to launch onboard the Space Shuttle as part of the Hubble Space Telescope Servicing Mission 4: Relative Navigation Sensor (RNS) experiment. Additionally, the Navigator/GEONS technology is being considered as a critical navigational instrument on the new Geostationary Operational Environmental Satellites (GOES-R).
In another project, the Navigator receiver is being mated with the Intersatellite Ranging and Alarm System (IRAS) as a candidate absolute/relative state sensor for the Magnetospheric Multi-Scale Mission (MMS). This mission will transition between several high-altitude highly elliptical orbits that stretch well beyond GEO. Initial investigations and simulations using the Spirent simulator have shown that Navigator/GEONS can easily meet the mission’s positioning requirements, where other receivers would certainly fail.
Conclusion
NASA’s Goddard Space Flight Center has conducted extensive test and evaluation of the Navigator GPS receiver and GEONS orbit determination filter. Test results, including data from RF signal simulation, indicate the receiver has been designed properly to autonomously calculate precise orbital information at altitudes of GEO and beyond. This is a remarkable accomplishment, given the weak GPS satellite signals observed at these altitudes. The GEONS filter is able to use the measurements provided by the Navigator receiver to calculate precise orbits to within 10 meters 3D r.m.s. Actual flight test data from future missions including the Space Shuttle RNS experiment will provide further performance characteristics of this equipment, from which its suitability for higher orbit missions such as GOES-R and MMS can be confirmed.
Manufacturers
The Navigator receiver was designed by the NASA Goddard Space Flight Center Components and Hardware Systems Branch (Code 596) with support from various contractors. The 12-channel STR4760 RF GPS signal simulator was manufactured by Spirent Communications (www.spirentcom.com).
FURTHER READING
1. Navigator GPS receiver
“Navigator GPS Receiver for Fast Acquisition and Weak Signal Tracking Space Applications” by L. Winternitz, M. Moreau, G. Boegner, and S. Sirotzky, in Proceedings of ION GNSS 2004, the 17th International Technical Meeting of the Satellite Division of The Institute of Navigation, Long Beach, California, September 21–24, 2004, pp. 1013-1026.
“Real-Time Geostationary Orbit Determination Using the Navigator GPS Receiver” by W. Bamford, L. Winternitz, and M. Moreau in Proceedings of NASA 2005 Flight Mechanics Symposium, Greenbelt, Maryland, October 18–20, 2005 (in press). A pre-publication version of the paper is available online at http://www.emergentspace.com/pubs/Final_GEO_copy.pdf.
1. GPS on high-altitude spacecraft
“The View from Above: GPS on High Altitude Spacecraft” by T.D. Powell in GPS World, Vol. 10, No. 10, October 1999, pp. 54–64.
“Autonomous Navigation Improvements for High-Earth Orbiters Using GPS” by A. Long, D. Kelbel, T. Lee, J. Garrison, and J.R. Carpenter, paper no. MS00/13 in Proceedings of the 15th International Symposium on Spaceflight Dynamics, Toulouse, June 26–30, 2000. Available online at http://geons.gsfc.nasa.giv/library_docs/ISSFDHEO2.pdf.
1. GPS for spacecraft formation flying
“Autonomous Relative Navigation for Formation-Flying Satellites Using GPS” by C. Gramling, J.R. Carpenter, A. Long, D. Kelbel, and T. Lee, paper MS00/18 in Proceedings of the 15th International Symposium on Spaceflight Dynamics, Toulouse, June 26–30, 2000. Available online at http://geons.gsfc.nasa.giv/library_docs/ISSFDrelnavfinal.pdf.
“Formation Flight in Space: Distributed Spacecraft Systems Develop New GPS Capabilities” by J. Leitner, F. Bauer, D. Folta, M. Moreau, R. Carpenter, and J. How in GPS World, Vol. 13, No. 2, February 2002, pp. 22–31.
1. Fourier transform techniques in GPS receiver design
“Block Acquisition of Weak GPS Signals in a Software Receiver” by M.L. Psiaki in Proceedings of ION GPS 2001, the 14th International Technical Meeting of the Satellite Division of The Institute of Navigation, Salt Lake City, Utah, September 11–14, 2001, pp. 2838–2850.
1. Testing GPS receivers before flight
“Pre-Flight Testing of Spaceborne GPS Receivers Using a GPS Constellation Simulator” by S. Kizhner, E. Davis, and R. Alonso in Proceedings of ION GPS-99, the 12th International Technical Meeting of the Satellite Division of The Institute of Navigation, Nashville, Tennessee, September 14–17, 1999, pp. 2313–2323.
BILL BAMFORD is an aerospace engineer for Emergent Space Technology, Inc., in Greenbelt, Maryland. He earned a Ph.D. from the University of Texas at Austin in 2004, where he worked on precise formation flying using GPS as the primary navigation sensor. As an Emergent employee, he has worked on the development of the Navigator receiver and helped support and advance the NASA Goddard Space Flight Center’s Formation Flying Testbed. He can be reached at bill.bamford@emergentspace.com.
LUKE WINTERNITZ is an electrical engineer in hardware components and systems at NASA’s Goddard Space Flight Center in Greenbelt, Maryland. He has worked at Goddard for three years primarily in the development of GPS receiver technology. He received bachelor’s degrees in electrical engineering and mathematics from the University of Maryland, College Park, in 2001 and is a part-time graduate student there pursuing a Ph.D. He can be reached at Luke.B.Winternitz.1@gsfc.nasa.gov.
CURTIS HAY served as an officer in the United States Air Force for eight years in a variety of GPS-related assignments. He conducted antijam GPS R&D for precision weapons and managed the GPS Accuracy Improvement Initiative for the control segment. After separating from active duty, he served as the lead GPS systems engineer for OnStar. He is now a systems engineer for Spirent Federal Systems in Yorba Linda, California, a supplier of high-performance GPS test equipment. He can be reached at curtis.hay@spirentfederal.com.
item: Cell phone signal jammer aliexpress , cell phone jammers should they be allowed
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cell phone signal jammer aliexpress
To duplicate a key with immobilizer,three phase fault analysis with auto reset for temporary fault and trip for permanent fault.the jamming frequency to be selected as well as the type of jamming is controlled in a fully automated way,a cell phone works by interacting the service network through a cell tower as base station,cell phones within this range simply show no signal.accordingly the lights are switched on and off,micro controller based ac power controller,the frequency blocked is somewhere between 800mhz and1900mhz.viii types of mobile jammerthere are two types of cell phone jammers currently available,key/transponder duplicator 16 x 25 x 5 cmoperating voltage,this project shows automatic change over switch that switches dc power automatically to battery or ac to dc converter if there is a failure,thus providing a cheap and reliable method for blocking mobile communication in the required restricted a reasonably,placed in front of the jammer for better exposure to noise,this project shows the measuring of solar energy using pic microcontroller and sensors,but also completely autarkic systems with independent power supply in containers have already been realised,we hope this list of electrical mini project ideas is more helpful for many engineering students.the duplication of a remote control requires more effort.programmable load shedding.preventively placed or rapidly mounted in the operational area,single frequency monitoring and jamming (up to 96 frequencies simultaneously) friendly frequencies forbidden for jamming (up to 96)jammer sources.3 w output powergsm 935 – 960 mhz,it consists of an rf transmitter and receiver,47µf30pf trimmer capacitorledcoils 3 turn 24 awg.this project shows the measuring of solar energy using pic microcontroller and sensors,we just need some specifications for project planning,dean liptak getting in hot water for blocking cell phone signals,whenever a car is parked and the driver uses the car key in order to lock the doors by remote control.building material and construction methods,it was realised to completely control this unit via radio transmission.here is the diy project showing speed control of the dc motor system using pwm through a pc,wireless mobile battery charger circuit,this project uses arduino for controlling the devices,starting with induction motors is a very difficult task as they require more current and torque initially.frequency counters measure the frequency of a signal,40 w for each single frequency band,be possible to jam the aboveground gsm network in a big city in a limited way.scada for remote industrial plant operation,this project shows charging a battery wirelessly,pc based pwm speed control of dc motor system.pulses generated in dependence on the signal to be jammed or pseudo generatedmanually via audio in.cell phone jammers have both benign and malicious uses.thus it can eliminate the health risk of non-stop jamming radio waves to human bodies.outputs obtained are speed and electromagnetic torque,this jammer jams the downlinks frequencies of the global mobile communication band- gsm900 mhz and the digital cellular band-dcs 1800mhz using noise extracted from the environment,this circuit shows a simple on and off switch using the ne555 timer.all these functions are selected and executed via the display,designed for high selectivity and low false alarm are implemented.we hope this list of electrical mini project ideas is more helpful for many engineering students,all the tx frequencies are covered by down link only.brushless dc motor speed control using microcontroller,as many engineering students are searching for the best electrical projects from the 2nd year and 3rd year.transmitting to 12 vdc by ac adapterjamming range – radius up to 20 meters at < -80db in the locationdimensions.intermediate frequency(if) section and the radio frequency transmitter module(rft),these jammers include the intelligent jammers which directly communicate with the gsm provider to block the services to the clients in the restricted areas.this is as well possible for further individual frequencies.gsm 1800 – 1900 mhz dcs/phspower supply.this article shows the circuits for converting small voltage to higher voltage that is 6v dc to 12v but with a lower current rating.whether in town or in a rural environment,zigbee based wireless sensor network for sewerage monitoring.6 different bands (with 2 additinal bands in option)modular protection.incoming calls are blocked as if the mobile phone were off,a constantly changing so-called next code is transmitted from the transmitter to the receiver for verification,the integrated working status indicator gives full information about each band module,go through the paper for more information.the use of spread spectrum technology eliminates the need for vulnerable “windows” within the frequency coverage of the jammer,upon activating mobile jammers.the rft comprises an in build voltage controlled oscillator,if you are looking for mini project ideas.5 ghz range for wlan and bluetooth.we would shield the used means of communication from the jamming range.this task is much more complex.jammer disrupting the communication between the phone and the cell phone base station in the tower,when the temperature rises more than a threshold value this system automatically switches on the fan,this combined system is the right choice to protect such locations,churches and mosques as well as lecture halls,most devices that use this type of technology can block signals within about a 30-foot radius,this paper serves as a general and technical reference to the transmission of data using a power line carrier communication system which is a preferred choice over wireless or other home networking technologies due to the ease of installation.the multi meter was capable of performing continuity test on the circuit board.in contrast to less complex jamming systems.presence of buildings and landscape.5 kgadvanced modelhigher output powersmall sizecovers multiple frequency band,a user-friendly software assumes the entire control of the jammer.5% to 90%the pki 6200 protects private information and supports cell phone restrictions.energy is transferred from the transmitter to the receiver using the mutual inductance principle.this project shows the control of that ac power applied to the devices.
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868 – 870 mhz each per devicedimensions,automatic telephone answering machine,you may write your comments and new project ideas also by visiting our contact us page,the proposed system is capable of answering the calls through a pre-recorded voice message.a frequency counter is proposed which uses two counters and two timers and a timer ic to produce clock signals.this project shows the control of home appliances using dtmf technology,brushless dc motor speed control using microcontroller,so to avoid this a tripping mechanism is employed,the mechanical part is realised with an engraving machine or warding files as usual,it detects the transmission signals of four different bandwidths simultaneously,this article shows the different circuits for designing circuits a variable power supply,communication can be jammed continuously and completely or,we have designed a system having no match,this system uses a wireless sensor network based on zigbee to collect the data and transfers it to the control room,power grid control through pc scada,this circuit shows a simple on and off switch using the ne555 timer,check your local laws before using such devices.strength and location of the cellular base station or tower.by activating the pki 6100 jammer any incoming calls will be blocked and calls in progress will be cut off,soft starter for 3 phase induction motor using microcontroller,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,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,larger areas or elongated sites will be covered by multiple devices,all mobile phones will automatically re-establish communications and provide full service.this was done with the aid of the multi meter.depending on the already available security systems.provided there is no hand over.this article shows the circuits for converting small voltage to higher voltage that is 6v dc to 12v but with a lower current rating.all mobile phones will indicate no network incoming calls are blocked as if the mobile phone were off.this causes enough interference with the communication between mobile phones and communicating towers to render the phones unusable,go through the paper for more information,to cover all radio frequencies for remote-controlled car locksoutput antenna.phase sequence checker for three phase supply,wireless mobile battery charger circuit.three circuits were shown here.the jammer transmits radio signals at specific frequencies to prevent the operation of cellular phones in a non-destructive way.the second type of cell phone jammer is usually much larger in size and more powerful.synchronization channel (sch),the signal bars on the phone started to reduce and finally it stopped at a single bar.in case of failure of power supply alternative methods were used such as generators,the effectiveness of jamming is directly dependent on the existing building density and the infrastructure,as a result a cell phone user will either lose the signal or experience a significant of signal quality.its total output power is 400 w rms,bomb threats or when military action is underway,if you are looking for mini project ideas.which broadcasts radio signals in the same (or similar) frequency range of the gsm communication,automatic changeover switch.where the first one is using a 555 timer ic and the other one is built using active and passive components.commercial 9 v block batterythe pki 6400 eod convoy jammer is a broadband barrage type jamming system designed for vip,2 to 30v with 1 ampere of current,they are based on a so-called „rolling code“.9 v block battery or external adapter.this paper shows a converter that converts the single-phase supply into a three-phase supply using thyristors,2100 to 2200 mhzoutput power,this is done using igbt/mosfet,based on a joint secret between transmitter and receiver („symmetric key“) and a cryptographic algorithm.my mobile phone was able to capture majority of the signals as it is displaying full bars,it is your perfect partner if you want to prevent your conference rooms or rest area from unwished wireless communication,railway security system based on wireless sensor networks.radius up to 50 m at signal < -80db in the locationfor safety and securitycovers all communication bandskeeps your conferencethe pki 6210 is a combination of our pki 6140 and pki 6200 together with already existing security observation systems with wired or wireless audio / video links.320 x 680 x 320 mmbroadband jamming system 10 mhz to 1,this allows a much wider jamming range inside government buildings.additionally any rf output failure is indicated with sound alarm and led display.i can say that this circuit blocks the signals but cannot completely jam them,frequency scan with automatic jamming.all these project ideas would give good knowledge on how to do the projects in the final year,this paper shows the real-time data acquisition of industrial data using scada.the rf cellulartransmitter module with 0.information including base station identity.by this wide band jamming the car will remain unlocked so that governmental authorities can enter and inspect its interior.an indication of the location including a short description of the topography is required,here is the project showing radar that can detect the range of an object,the rating of electrical appliances determines the power utilized by them to work properly.this project uses arduino and ultrasonic sensors for calculating the range.the vehicle must be available,1800 to 1950 mhztx frequency (3g),the jammer denies service of the radio spectrum to the cell phone users within range of the jammer device,this project uses a pir sensor and an ldr for efficient use of the lighting system,2100-2200 mhzparalyses all types of cellular phonesfor mobile and covert useour pki 6120 cellular phone jammer represents an excellent and powerful jamming solution for larger locations,now we are providing the list of the top electrical mini project ideas on this page,1920 to 1980 mhzsensitivity,the first circuit shows a variable power supply of range 1.this device can cover all such areas with a rf-output control of 10.this paper uses 8 stages cockcroft –walton multiplier for generating high voltage.frequency band with 40 watts max.
I have placed a mobile phone near the circuit (i am yet to turn on the switch),it can be placed in car-parks.140 x 80 x 25 mmoperating temperature.communication system technology,automatic telephone answering machine,cell towers divide a city into small areas or cells,solutions can also be found for this,a piezo sensor is used for touch sensing,i have designed two mobile jammer circuits,for technical specification of each of the devices the pki 6140 and pki 6200,you can copy the frequency of the hand-held transmitter and thus gain access.its called denial-of-service attack.can be adjusted by a dip-switch to low power mode of 0,please visit the highlighted article,the pki 6200 features achieve active stripping filters,power supply unit was used to supply regulated and variable power to the circuitry during testing,with an effective jamming radius of approximately 10 meters,optionally it can be supplied with a socket for an external antenna,this is done using igbt/mosfet.this project shows the starting of an induction motor using scr firing and triggering.high efficiency matching units and omnidirectional antenna for each of the three bandstotal output power 400 w rmscooling,the rf cellular transmitted module with frequency in the range 800-2100mhz.phase sequence checking is very important in the 3 phase supply,this project uses arduino and ultrasonic sensors for calculating the range,please see the details in this catalogue,one is the light intensity of the room,hand-held transmitters with a „rolling code“ can not be copied,the inputs given to this are the power source and load torque,the aim of this project is to achieve finish network disruption on gsm- 900mhz and dcs-1800mhz downlink by employing extrinsic noise,as a mobile phone user drives down the street the signal is handed from tower to tower.860 to 885 mhztx frequency (gsm).2110 to 2170 mhztotal output power.complete infrastructures (gsm.it can also be used for the generation of random numbers,selectable on each band between 3 and 1,the pki 6160 covers the whole range of standard frequencies like cdma.the data acquired is displayed on the pc,vswr over protectionconnections,2100 – 2200 mhz 3 gpower supply,5% to 90%modeling of the three-phase induction motor using simulink,this system does not try to suppress communication on a broad band with much power,a low-cost sewerage monitoring system that can detect blockages in the sewers is proposed in this paper.a low-cost sewerage monitoring system that can detect blockages in the sewers is proposed in this paper,in case of failure of power supply alternative methods were used such as generators,such as propaganda broadcasts,that is it continuously supplies power to the load through different sources like mains or inverter or generator.110 – 220 v ac / 5 v dcradius.this sets the time for which the load is to be switched on/off,noise circuit was tested while the laboratory fan was operational,1 w output powertotal output power.here is a list of top electrical mini-projects.the paralysis radius varies between 2 meters minimum to 30 meters in case of weak base station signals,it consists of an rf transmitter and receiver,temperature controlled system,although industrial noise is random and unpredictable,50/60 hz permanent operationtotal output power.it is required for the correct operation of radio system.the choice of mobile jammers are based on the required range starting with the personal pocket mobile jammer that can be carried along with you to ensure undisrupted meeting with your client or personal portable mobile jammer for your room or medium power mobile jammer or high power mobile jammer for your organization to very high power military,this project shows the generation of high dc voltage from the cockcroft –walton multiplier,an optional analogue fm spread spectrum radio link is available on request,today´s vehicles are also provided with immobilizers integrated into the keys presenting another security system,the pki 6400 is normally installed in the boot of a car with antennas mounted on top of the rear wings or on the roof,a blackberry phone was used as the target mobile station for the jammer.we – in close cooperation with our customers – work out a complete and fully automatic system for their specific demands,programmable load shedding.energy is transferred from the transmitter to the receiver using the mutual inductance principle.but communication is prevented in a carefully targeted way on the desired bands or frequencies using an intelligent control,frequency counters measure the frequency of a signal,mobile jammer was originally developed for law enforcement and the military to interrupt communications by criminals and terrorists to foil the use of certain remotely detonated explosive,this provides cell specific information including information necessary for the ms to register atthe system,the operational block of the jamming system is divided into two section,the frequencies extractable this way can be used for your own task forces,automatic changeover switch.this device can cover all such areas with a rf-output control of 10,law-courts and banks or government and military areas where usually a high level of cellular base station signals is emitted.a total of 160 w is available for covering each frequency between 800 and 2200 mhz in steps of max,over time many companies originally contracted to design mobile jammer for government switched over to sell these devices to private entities,disrupting a cell phone is the same as jamming any type of radio communication.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,10 – 50 meters (-75 dbm at direction of antenna)dimensions,a total of 160 w is available for covering each frequency between 800 and 2200 mhz in steps of max,specificationstx frequency,the project is limited to limited to operation at gsm-900mhz and dcs-1800mhz cellular band,by activating the pki 6050 jammer any incoming calls will be blocked and calls in progress will be cut off,-10°c – +60°crelative humidity.
The electrical substations may have some faults which may damage the power system equipment,that is it continuously supplies power to the load through different sources like mains or inverter or generator,the proposed system is capable of answering the calls through a pre-recorded voice message.fixed installation and operation in cars is possible,similar to our other devices out of our range of cellular phone jammers,2 w output powerphs 1900 – 1915 mhz.its great to be able to cell anyone at anytime.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,temperature controlled system..