Communications: directive radio wave systems and devices (e.g. – Directive – Utilizing correlation techniques
Reexamination Certificate
2000-09-26
2002-05-21
Phan, Dao (Department: 3662)
Communications: directive radio wave systems and devices (e.g.,
Directive
Utilizing correlation techniques
C342S372000, C342S383000
Reexamination Certificate
active
06392596
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to the Global Positioning System (GPS) and more particularly to GPS reception in an interference environment.
2. Description of the Related Art
Numerous guidance and navigation systems benefit from use of the GPS which provides a wealth of information such as latitude, longitude, height, velocity and the exact time. The GPS constellation contains 24 satellites which are distributed throughout 6 different orbits. GPS signals are at carrier frequencies L
1
(1575.42 MHz) and L
2
(1227.60 MHz) and use spread spectrum signals with 1.023 Mbps binary phase shift keying (BPSK) modulation for a “short” coarse/acquisition (C/A) code and 10.23 Mbps modulation for a “long” precision (P) code.
With right-hand circular polarization, each GPS satellite transmits the following three signals: the C/A code modulated on the L
1
carrier frequency with a 1 millisecond repetition rate, the P code modulated on the L
1
carrier with a weekly repetition period and the P code modulated on the L
2
carrier with a weekly repetition period.
The GPS constellation's design insures that 6 to 11 satellites are in view from any point on the earth's surface at any given time. Because of the GPS signal design, two-dimensional and three-dimensional positions can be determined with the signals from just three and four satellites respectively. Accordingly, GPS receivers typically have the capability of automatically selecting three or four of the satellites in view based upon their received signal strength and Position Dilution of Precision (PDOP).
A number of undesirable interference sources (e.g., deliberate electronic countermeasures, RF electromagnetic pollution, clutter scatter returns and nature noise) can cause a GPS receiver to be ineffective or unreliable. Receiver failure is generally due to missing synchronization in the spread-spectrum Pseudo Random Noise (PRN) code.
Accordingly, adaptive antenna arrays have been proposed in which knowledge of each element's received signal is used to modify those signals with weights (e.g., phase weights) that generate a null in the interfering signal's direction.
Various adaptive array systems are based on gradient-based algorithms which estimate the antenna's output-power gradient. Because processed signals from each element of the array are typically required for gradient computation, these receiving systems are often said to use a “multiport technique”. In order to compute gradient of power, or correlation or other performance, the signal from every element must be accessible in these systems, i.e., a separate receiving channel is required for every element in the antenna array. Multiport techniques therefore require a separate coherent receiver channel for each element in the antenna array.
This is illustrated in
FIG. 1
which shows an exemplary multiport structure
20
that has an array
22
of N antenna elements
24
. Each element
24
feeds a different receiver channel
26
that includes an adjustable weighting element (e.g., a phase shifter)
28
, a low noise amplifier
30
, a down converter
32
for down converting the signal frequency from L band to baseband (or IF band) and a pair of analog-to-digital converters (ADC)
34
for partitioning the downconverted signal into I/Q components.
The digitized I/Q signals are coupled to a digital signal processor (DSP)
36
which performs optimal weight computations that require up to n(n+1) auto-correlation and cross-correlations and an n×n inverse matrix computation. A weight controller
38
then feeds the computed phase shifts back to the phase shifters
28
.
An exemplary multiport technique is described in U.S. Pat. No. 5,694,416 (issued Dec. 2, 1997 to Russell K. Johnson) and another is shown in U.S. Pat. No. 5,471,220 (issued on Nov. 28, 1995 to David E. Hammers et al.) which illustrates a microwave packaging scheme that includes a coplanar section, fiber optical network, a plurality of adaptive beam processors, a fiber optical network, one or more signal processing modules and a set of microprocessors. In the coplanar section, a “sandwich style” package includes 3 layers: an antenna layer consisting of a plurality of elements, a transceiver layer consisting of a plurality of transceivers, and a beam forming layer.
U.S. Pat. No. 5,712,641 (issued on Jan. 27, 1998, to Mario M. Casabona et al.) describes an adaptive cross polarization interference cancellation system for GPS signals. It is based on dissimilarity between the right hand circular polarization of the GPS signal and the polarization of the interference signals. An orthogonally-polarized antenna system decomposes the received GPS signal into vertical-polarization and horizontal-polarization signals. Both are fed to an adaptive antenna feeding system which is controlled by an interference detection circuit and the resultant cross polarization attenuates the interference signals.
A reception technique which utilizes an analog to digital converter (ADC) prior to GPS signal processing is described in U.S. Pat. No. 5,347,284 (issued on Sep. 13, 1994, to John P. Volpi et al.). The ADC uses 4 level coding and full zone processing. A threshed detector senses the difference of a probability density function (PDF) in time distribution between the GPS signals' spread spectrum and continuous wave (CW) signals. For the CW signal, The PDF of the CW signal has a saddle shape (a falling off between two peak ending values) whereas that of the GPS signal is nearly uniform. Attenuating the digitized data in the vicinity of the peak ending values provides a degree of immunity to CW interference.
Although these conventional reception methods may improve reception of GPS signals in interference environments, they typically are hardware intensive (e.g., U.S. Pat. Nos. 5,694,416, 5,471,220 and 5,712,641) or limited to particular interference signals (e.g., U.S. Pat. No. 5,347,284).
SUMMARY OF THE INVENTION
The present invention is directed to methods for removing multiple interference signals from GPS signals without requiring:
a) complex gradient computations,
b) prior knowledge of interference-signal structure, or
c) an inordinate increase in software and hardware complexity as the number of interference signals increases.
These goals are achieved with adaptive nulling methods that combine orthogonal projection of sub-optimal weight vectors into an orthonormal weight base with an accelerated coefficient-searching process. Because they facilitate the use of single-output-port antennas and can be applied to any number of array elements, these methods reduce hardware complexity and system cost.
In particular, an optimal weight vector comprises the phases of array signals and is approximated by a linear combination of a set of orthonormal basis vectors and a corresponding set of coefficients. The coefficients are obtained by monitoring the single-output-port power while an intelligent controller controls the weights of all array elements simultaneously. In an exemplary embodiment, the orthonormal basis vectors are constructed from orthonormal radial and azimuth vector bases.
The methods do not require prior knowledge of interference-signal structures and, because of the uncoupled nature of the orthonormal basis vectors, they facilitate the simultaneous change of all phases so that the process rapidly converges to an optimal weight vector.
The novel features of the invention are set forth with particularity in the appended claims. The invention will be best understood from the following description when read in conjunction with the accompanying drawings.
REFERENCES:
patent: 3806924 (1974-04-01), Applebaum
patent: 4263617 (1981-04-01), Chemin et al.
patent: 4338605 (1982-07-01), Mims
patent: 4931977 (1990-06-01), Klemes
patent: 5019793 (1991-05-01), McNab
patent: 5033110 (1991-07-01), Harman
patent: 5068668 (1991-11-01), Tsuda et al.
patent: 5347284 (1994-09-01), Volpi et al.
patent: 5471220 (1995-11-01), Hammers
patent: 5530927 (1996-06-01),
Lin Jian-Jin
Lin Zhen Biao
Robin Seymour
Koppel, Jacobs Patrick & Heybl
Phan Dao
Sensor Systems, Inc.
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