Maxim MAX2741

The Maxim 2741 is an integrated L1 (civilian frequency) GPS receiver first announced in 2005.

The MAX2741 L1-band GPS receiver IC offers a high-performance, compact solution for mobile handsets, PDAs, and automotive applications. Total voltage gain of 80dB and a 4.7dB cascaded noise figure can pro-vide receiver sensitivity for applications requiring -185dBW for indoor tracking solutions.

This dual-conversion receiver downconverts the 1575.42MHz GPS signal to a 37.38MHz first IF, and then a 3.78MHz second IF. An integrated 2- or 3-bit ADC (1- bit SIGN, 1- or 2-bit MAG selectable) samples the sec-ond IF and outputs the digitized signals to the baseband processor.

The integrated synthesizer offers the flexibility in fre-quency planning to allow a single board design to be employed for reference frequencies from 2MHz to 26MHz. The integrated reference oscillator allows either TCXO or crystal operation.

The receiver runs from a 2.7V to 3.0V supply, and draws only 30mA when active. It is offered in a 28-pin thin QFN package, and is specified for -40°C to +85°C at 3V.

Maxim produced an evaluation kit and a USB form-factor device called the MAX2741USBDONGLE+.

I am looking for software (with source code) that can communicate with this USB device, at a minimum to pull I/Q samples.

INSIDE GNSS

September 2006

Maxim-Philips Partner on Chipset

One of the more interesting products (and alliances) to appear this summer is the coupling of Maxim Integrated Product's MAX2741 GPS RFIC and Royal Philips Electronics. Spot GPS software designed to operate on a host application processor

The combination eliminates the need for a baseband IC and reuses other system resources such as a reference clock. The appears likely to reduce size, power requirements, and bill of materi- als (BOM) of products and systems incorporating the RFIC/software, according to the company, which has cited a sub-$4 per unit price in large volumes.

Operating in both autonomous (unassisted) and assisted modes, the software solution can provide fixes every second for applications such as automotive tracking. According to the Sunnyvale, California-based company, the algorithm can also be tuned to support pedestrian or indoor use, tar- geting integration into such mobile devices such as cellular phones, PDAs, digital cameras, MP3 players, laptops, and portable DVD players.

The first product based on this GPS solution is a reference design for an USB accessory for laptops, which in a simple application could transform the computer into a large-screen navigation device, Maxim suggests.

NASA TECH BRIEFS

NASA Tech Briefs Article

GPS Receiver RF Front-End Enables Use of a Laptop PC for Soft Baseband Processing

Friday, 24 August 2007

Software techniques for use in the global positioning system (GPS)1,2 have recently captured the growing interest of communication and navigation engineers. Thanks to very-largescale integration (VLSI) development, powerful CPUs and DSPs are now capable of detecting and decoding GPS signals in real time using software. The resulting software-based GPS receivers offer considerable flexibility in modifying settings to accommodate new applications without hardware redesign, using the same board design for different frequency plans, and implementing future upgrades.

The CPU inside most of today's laptop computers has plenty of performance to meet the real-time decoding needs. By using a chip like the MAX2741 GPS receiver RF front-end, a simple USB dongle or PCIexpress minicard can be used to add low-cost GPS capability to a laptop PC, by letting the PC execute the baseband decoding in software, eliminating the cost of the baseband ASIC typically required in standalone GPS systems.

Figure 1. In a software GPS receiver, the captured RF signal must be amplified, mixed down in frequency, and then digitized. The RF front-end of a software-based GPS receiver first amplifies the weak incoming signal with a low-noise amplifier (LNA), and then downconverts the signal to a low intermediate frequency (IF) of approximately 4 MHz (Figure 1). This downconversion is accomplished by mixing the input RF signal with the local oscillator signal using one or two mixers. The resulting analog IF signal is converted to a digital IF signal by the analog-todigital converter (ADC).

All those functions - LNA, mixer, and ADC - have been integrated into the MAX2741, thus significantly reducing the development time for applications. A two-stage receiver amplifies the incident 1575.42-MHz GPS signal, downconverts it to a first IF of 37.38 MHz, further amplifies it, and then downconverts to a second IF of 3.78 MHz. An internal 2- or 3-bit ADC (selectable as a 1-bit sign with a 1- or 2-bit magnitude) samples the second IF and outputs a digitized signal to the baseband processor. The integrated frequency synthesizer enables flexible frequency planning, allowing the same board to implement many popular reference frequencies between 2 and 26 MHz with just a change of settings. The integrated reference oscillator enables operation with either a crystal or a temperature-compensated crystal oscillator (TCXO).

A simple USB dongle reference design based on the MAX2741 and a Cypress Semiconductor USB controller operates from a 24-MHz crystal reference (to match the clock required by the USB controller). It also employs two MAX8510 LDOs to regulate the DC supply. A 3-wire (SPI) digital bus is used to program the registers of the MAX2741. This reference design allows a hardwired connection of the active antenna onto the PCB, thus integrating it into the design. It also includes additional circuitry to turn off the antenna during shutdown mode for USB compliance. The MAX2741 also includes an integrated synthesizer that allows a single board design to be employed for reference frequencies up to 26 MHz. The integrated reference oscillator allows either TCXO or crystal operation.

Before examining the design of the USB or PCIe hardware, let's review a little of the basic theory for software GPS receivers. For the decoding of navigation messages and position calculations, the interested reader can refer to James Bao-Yen Tsui's book, Fundamentals of Global Positioning System Receivers: A Software Approach.

GPS Basics

A GPS system consists of 24 space satellites or space vehicles (each identified by a unique PRN code), a ground-control station, and user equipment (receivers). For civilian GPS applications, the satellites communicate over the L1 band located at 1.57542 GHz. A GPS receiver requires line-of-sight .visibility. of at least four satellites to establish a reliable position. Acquisition and tracking of the signals is very complex, because each one varies with time as well as receiver location.

Traditional GPS receivers implement acquisition, tracking, and bit-synchronization operations in an ASIC, but a software GPS receiver provides flexibility by implementing those blocks in software rather than hardware. By simplifying the hardware architecture, software makes the receiver smaller, cheaper, and more power-efficient. You can write the software in C/C++, MATLAB®, and other languages, and port it into all operating systems (embedded OS, PC, Linux, and DSP platforms). Thus, software GPS receivers offer the greatest flexibility for mobile handsets, PDAs, and similar applications.

Figure 2. Typical adapter configurations for the USB dongle (a), and the PCIe minicard (b) showthe simple, low bill of materials design for either option. For laptop computers, designers can opt to design either a USB "dongle" that can work with any laptop with USB ports, or for newer laptops that have a PCIexpress minicard connector, they can put the RF front-end on the PCIe minicard and embed the card in the PC (Figure 2a, b). The PCIe minicard interface includes a USB port, so the design of the front-end adapter is similar for both USB and the PCIe minicards. The main difference is in some of the powermanagement logic required for the PCIe support and to deal with the different DC voltages (3.3-V for PCIe and 5-V for external USB ports).

The USB dongle solution can be simple, with just the MAX2741, a counter, and the USB interface controller needed to capture the signal convert it to digital and send it to the host PC. Software running on the host PC then performs all the baseband functions and displays the location on the PC screen.

This article will only examine the civilian GPS signal on the well-known L1 band located at 1.57542 GHz. The GPS system is actually a simple spreadspectrum communication system4. First, the 50-bps navigation message is repeated 20 times to produce a 1,000- bps bit stream. The repeated signal is then spread by a unique C/A code with a length of 1,023 chips (a chip is the rate at which the pseudorandom noise code is applied). The result is a baseband signal of 1.023 megabits per second (Mbps). Hence, the 43-dB processing gain (G) of the GPS system permits it to resolve a signal well below the thermal noise level.

Each satellite is assigned a unique C/A code, also called a gold code5. Because the gold code exhibits excellent auto- and cross-correlation properties, it is widely used in CDMA communication systems such as WCDMA, cdma2000®, and others. The baseband signal is modulated with binary phase-shift keying (BPSK), and upconverted to the L1 band for transmission.

Acquiring the Signal

Because GPS is a CDMA communications system, the receiver must synchronize the pseudorandom noise (PRN) code as a prerequisite to demodulating the data. Code synchronization is usually achieved in two steps: code acquisition for the coarse-code alignment, and code-phase tracking for the fine alignment6. More explicitly, a GPS receiver must first determine whether it has lineof- sight visibility to certain satellites. As we know, each satellite is distinguished by a unique C/A code. When the satellite is visible, acquisition determines the signal.s frequency and code phase, which in turn establishes the corresponding demodulation parameters. The received-signal frequency varies due to the Doppler effect7, which causes the frequency to deviate from its nominal value by 5 kHz to 10 kHz, depending on the speed of the satellite with respect to the receiver.

In the receiver, the GPS signal is first downconverted to in-phase and quadrature (I and Q) components. A pair of IQ correlators then correlates the I and Q baseband signals with the locally generated PRN sequence. After integrating over the duration of one bit, the I-Q correlator outputs are summed to provide an output-decision variable.

Whenever the decision variable exceeds a certain threshold value, the system assumes the corresponding acquisition was successful and proceeds to the tracking mode. Otherwise, the relative phase of the locally generated PRN sequence and the oscillator frequency are adjusted to update the decision variable, and the above process is repeated. The simple logic structure of the serialsearch method makes it feasible for implementation in an ASIC, but for software implementations it is not practical because the search space is huge.

Assuming the system tolerates a 500- Hz carrier-frequency offset and the Doppler frequency is 10 kHz, the search space for a software implementation is roughly 2 × (10,000/500) × 1023 = 40,920. Obviously, a serial-search acquisition would be difficult in software.

Another acquisition method, called frequency-domain parallel code-phase acquisition, is less complex to implement with software. In this method, the Doppler-frequency and code-phase searches are combined into one search, which, after an FFT transform of the PRN code, reflects all code-phase information into the frequency domain. We then need only to search the space over the Doppler-frequency offset, thereby implementing a fast and effective software search.

The system implements this by first multiplying the incoming signal with the locally generated sine and cosine carrier waves respectively (the I and Q signal components). The I and Q components are then combined as a complex input to an FFT block. The result of this Fourier transform is multiplied with the conjugate of a PRN code's FFT transform (the PRN generator generates a code with zero-code phase). In practice, the FFT operation and generation of PRN code can be tabulated to reduce computation complexity.

Finally, the product of the incoming signal and local code, which represents the correction between the incoming and carrier frequencies, is applied to an inverse Fourier transform whose squared output feeds back to the decision logic. The FFT-based frequency domain has proven to be a low consumer of computation. For the example mentioned earlier, the complexity of acquisition is roughly 20,000/500 = 40 FFT operations.

Thus, the serial-search method has the simple logic and control architecture necessary for a convenient ASIC implementation. The huge search space, however, imposes complexity on the software algorithm. The serial-search method is therefore not a good choice for software GPS receivers. In contrast, the low complexity of the parallel-code acquisition method makes it ideal for the software implementation. Its logic architecture, however, is far more complex than that of the serial-search method, making it difficult to implement in an ASIC.

Tracking Refines Alignment

Figure 3. The DLL circuit multiplies the incoming signal by three local replicas of the PRN code (positioned in time at ± 0.5 chip),which represent early, prompt, and late arrivals with respect to theincoming signal. The one with the highest correlation value is then selected and retained.

Acquisition establishes a coarse alignment of the GPS signal's frequency and code-phase parameters. The purpose of tracking, therefore, is to refine this alignment so the system can demodulate the data with exact code-phase and frequency information. Tracking includes code-phase tracking and carrier-frequency tracking.

The DLL circuit multiplies the incoming signal by three local replicas of the PRN code (positioned in time at ±0.5 chip), which represent early, prompt, and late arrivals with respect to the incoming signal. After integration, each of these signals represents a correlation between the incoming signal and a local replica. The one with the highest correlation value is then selected and retained (Figure 3). Carrier-frequency tracking is carried out by a phase-lock loop (PLL) or Costas loop8. The purpurpose of carrier tracking is to tune the locally generated frequency to the exact frequency of the incoming signal.

After acquisition and tracking have established the initial synchronization, the system can decode the navigation bits. Data demodulation begins by despreading the 1.023-Mbps input signal to a 1,000-bps bit stream. Bit synchronization is then invoked to recover the 50-bps information from the 1,000-bps stream. For bit synchronization, we first need to identify the beginning of a bit in time. This is accomplished by finding the zero-crossing edge (at 0V), which indicates the beginning of a bit. When that edge is known, we can partition the 1,000-bps input stream at 20-ms intervals, knowing that the duration of a navigation data message (50 bits) is 20 ms. Finally, the bit samples in a 20-ms interval are summed and averaged to decode the navigation data.

The software that runs on the PC is the swGPS. Spot Version 2 from NXP's Software division. It can turn a notebook PC into a powerful location device, supporting navigation and a wealth of location- based services. The GPS front-end streams digitized IF data into the notebook via the industry-standard USB 2.0 interface. The Spot software uses the input to calculate a position fix and subsequently, to perform tracking. The code footprint on the host PC is about 750 kbytes and the software needs about 27 Mbytes of workspace when fed by a 12 Mbit/s GPS front end data stream. (For more information on the software, go to www.software.nxp.com or www.swgps.com.)

[NOTE: The web links mentioned in this article are out of date.]

A virtual COM port created by the software allows the software to link to a wealth of existing navigation and location applications. The software output interface conforms to NMEA 0183 and the application can run on Microsoft.s Windows XP and Vista operating systems. Additionally, the software can handle all available assistance data, whether supplied via industrystandard protocols or proprietary customer interfaces. When the software runs on a 1-GHz Pentium M system, the average processor load when tracking is 13%; when run on a Pentium Core Duo processor running at 2.18 GHz, the processor load is just 4%, both when performing updates every second.

Software GPS techniques provide a high level of flexibility and simplicity for many potential applications. To support these possibilities, the MAX2741 RF front-end provides flexibility in frequency planning for software GPS receivers and traditional hardware implementations as well. Of course, every solution has its pros and cons . software GPS receivers require a high-performance processor and moderate amounts of memory.

This article was written by David Weber, Strategic Applications Engineer, at Maxim Integrated Products Inc. in Sunnyvale, CA.

(MATLAB is a registered trademark of The MathWorks; cdma2000 is a registered trademark of the Telecommunications Industry Association.)

References

[1] E. Kaplan. Understanding GPS: Principles and Applications. 2nd ed. Artech House Publishers, 1996.
[2] J. Bao-Yen Tsui. Fundamentals of Global Positioning System Receivers: A Software Approach. 2nd ed. John Wiley & Sons Inc., 2004.
[3] Ibid. [4] A. Viterbi. Principles of Spread Spectrum Communications. Addison Wesley Longman Publishing Co., Inc., 1995.
[5] R. Gold, Co-optimal binary sequences for spread spectrum multiplexing, IEEE Transactions on Information Theory. Vol. IT-13. October 1967. pp. 619.621.
[6] R. E. Ziemer and R. L. Peterson. Digital Communications and Spread Spectrum Systems. New York: Macmillan Publishing Company, 1985.
[7] J. G. Proakis. Digital Communications. 4th ed. Mc-Graw Hill College, 2000.
[8] Ibid.


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Last revised February 1, 2014