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GPS signals

About: GPS signals is a research topic. Over the lifetime, 6150 publications have been published within this topic receiving 84454 citations.


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BookDOI
24 Nov 2004
TL;DR: This book discusses the history and present situation of the GPS system, as well as some of the technologies and subjects related to receiver hardware and software used in the system.
Abstract: Preface. Preface to the First Edition. Chapter 1. Introduction. Chapter 2. Basic GPS Concept. Chapter 3. Satellite Constellation. Chapter 4. Earth-Centered, Earth-Fixed Coordinate System. Chapter 5. GPS C/A Code Signal Structure. Chapter 6. Receiver Hardware Considerations. Chapter 7. Acquisition of GPSb C/A Code Signals. Chapter 8. Tracking GPS Signals. Chapter 9. GPS Software Receivers. Chapter 10. Acquisition of Weak Signals. Chapter 11. Tracking Weak Signals. Chapter 12. GPS Receiver-Related Subjects. Index.

985 citations

Journal ArticleDOI
TL;DR: A theoretical model that describes the power of a scattered GPS signal as a function of geometrical and environmental parameters has been developed, suggesting mapping of the wave-slope probability distribution in a synthetic-aperture-radar (SAR) fashion to allow more accurate measurements of wind velocity and wind direction.
Abstract: A theoretical model that describes the power of a scattered Global Positioning System (GPS) signal as a function of geometrical and environmental parameters has been developed. This model is based on a bistatic radar equation derived using the geometric optics limit of the Kirchhoff approximation. The waveform (i.e., the time-delayed power obtained in the delay-mapping technique) depends on a wave-slope probability density function, which in turn depends on wind. Waveforms obtained for aircraft altitudes and velocities indicate that altitudes within the interval 5-15 km are the best for inferring wind speed. In some regimes, an analytical solution for the bistatic radar equation is possible. This solution allows converting trailing edges of waveforms into a set of straight lines, which could be convenient for wind retrieval. A transition to satellite altitudes, together with satellite velocities, makes the peak power reduction and the Doppler spreading effect a significant problem for wind retrieval based on the delay-mapping technique. At the same time, different time delays and different Doppler shifts of the scattered GPS signal could form relatively small spatial cells on sea surface, suggesting mapping of the wave-slope probability distribution in a synthetic-aperture-radar (SAR) fashion. This may allow more accurate measurements of wind velocity and wind direction.

826 citations

Patent
08 Oct 1996
TL;DR: A GPS receiver in one embodiment includes an antenna which receives GPS signals at an RF frequency from in view satellites; a downconverter coupled to the antenna for reducing the RF frequency of the received GPS signals to an intermediate frequency (IF); a digitizer coupled to GPS signals and sampling the signals at a predetermined rate to produce sampled IF GPS signals as discussed by the authors.
Abstract: A GPS receiver in one embodiment includes an antenna which receives GPS signals at an RF frequency from in view satellites; a downconverter coupled to the antenna for reducing the RF frequency of the received GPS signals to an intermediate frequency (IF); a digitizer coupled to the downconverter and sampling the IF GPS signals at a predetermined rate to produce sampled IF GPS signals; a memory coupled to the digitizer storing the sampled IF GPS signals (a snapshot of GPS signals); and a digital signal processor (DSP) coupled to the memory and operating under stored instructions thereby performing Fast Fourier Transform (FFT) operations on the sampled IF GPS signals to provide pseudorange information. These operations typically also include preprocessing and post processing of the GPS signals. After a snapshot of data is taken, the receiver front end is powered down. The GPS receiver in one embodiment also includes other power management features and includes, in another embodiment the capability to correct for errors in its local oscillator which is used to sample the GPS signals. The calculation speed of pseudoranges, and sensitivity of operation, is enhanced by the transmission of the Doppler frequency shifts of in view satellites to the receiver from an external source, such as a basestation in one embodiment of the invention.

804 citations

Patent
04 Dec 1996
TL;DR: In this paper, a precision carrier frequency signal for calibrating a local oscillator of a GPS receiver which is used to acquire GPS signals was used to determine approximate Doppler data for satellites in view of the remote GPS receiver.
Abstract: A precision carrier frequency signal for calibrating a local oscillator of a GPS receiver which is used to acquire GPS signals. The precision carrier frequency signal is used to calibrate the local oscillator such that the output of the local oscillator, which is used to acquire GPS signals, is modified by a reference signal generated from the precision carrier frequency signal. The GPS receiver locks to this precision carrier frequency signal and generates the reference signal. In another aspect of the invention, satellite almanac data is transmitted to a remote GPS receiver unit from a basestation via a communication link. The remote GPS receiver unit uses this satellite almanac data to determine approximate Doppler data for satellites in view of the remote GPS receiver unit.

679 citations

Journal ArticleDOI
TL;DR: In this paper, the authors review the impact of scintillations on GPS receiver design and use and present a review of GPS and ionospheric scintillation for scientists interested in space weather.
Abstract: [1] Ionospheric scintillations are one of the earliest known effects of space weather. Caused by ionization density irregularities, scintillating signals change phase unexpectedly and vary rapidly in amplitude. GPS signals are vulnerable to ionospheric irregularities and scintillate with amplitude variations exceeding 20 dB. GPS is a weak signal system and scintillations can interrupt or degrade GPS receiver operation. For individual signals, interruption is caused by fading of the in-phase and quadrature signals, making the determination of phase by a tracking loop impossible. Degradation occurs when phase scintillations introduce ranging errors or when loss of tracking and failure to acquire signals increases the dilution of precision. GPS scintillations occur most often near the magnetic equator during solar maximum, but they can occur anywhere on Earth during any phase of the solar cycle. In this article we review the subject of GPS and ionospheric scintillations for scientists interested in space weather and engineers interested in the impact of scintillations on GPS receiver design and use.

534 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202338
202288
2021122
2020222
2019231
2018272