Left-hand circular polarized antenna for use with GPS systems

Communications: radio wave antennas – Antennas – Microstrip

Reexamination Certificate

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Details

C343S713000, C343S797000

Reexamination Certificate

active

06211823

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Technical Field
The present invention pertains to an antenna; more particularly the present invention pertains to a left-hand circular polarized GPS antenna used to receive space-based satellite GPS signals after reflecting off of a surface an odd number of times.
2. History of Related Art
Polarization is a description of how the direction of the electric field vector changes within an electromagnetic wave at a fixed point in space over time. If the wave is propagating in the positive z-direction, the electric field vector at a fixed point, for example at z=0.0, can be expressed in the following general form:
E
z=0,t
=&dgr;
x
E
o
cos(&ohgr;
t
)+&dgr;
y
AE
o
cos(&ohgr;
t
+&phgr;)
Mathematically, linear and circular polarization are special cases of elliptical polarization. Consider two electric-field vectors at right angles to each other propogating in the same direction. The frequencies are the same, but the magnitudes and face angles vary. If either one or the other of the magnitudes is zero, linear polarization results. If the magnitudes are the same and the phase angle between the two vectors (in time) is 90 degrees, circular polarization results. Of course, any combination between these two limits gives elliptical polarization.
The ideal antenna for use with random polarization is one with a circularly polarized radiation pattern. Polarization sense is a critical factor, especially when satellites are used to propagate signals, since the receiving antenna must be of the same polarity as the transmitting antenna for proper reception. In the case of GPS satellites, the most common transmitted signal is the right hand circular polarized signal. This occurs when the values for the general equation above include A=1 and &phgr;=−&pgr;/2, thus:
E
z=0,t
=&dgr;
x
E
o
cos(&ohgr;
t
)+&dgr;
y
E
o
cos(&ohgr;
t
−&pgr;/2)
The x and y components of the electrical field in this case have the same magnitude, and oscillate 90 degrees out of phase.
The signal emanating from the space-based satellite GPS system is right-hand circular polarized, and is intended to be received by a Right-Hand Circular Polarized (RHCP) antenna. However, optimal reception of a RHCP signal by a RHCP antenna requires that the antenna be in direct line-of-sight with the satellite. If the RHCP signal reflects off of a surface before striking the antenna, the polarity will be reversed (to Left-Hand Circular Polarized (LHCP)) with an attendant loss of signal strength.
The characteristic equation for a Left-Hand Circularly Polarized signal results when A=1 and &phgr;=&pgr;/2, thus:
E
z=0,t
=&dgr;
x
E
o
cos(
wt
)+&dgr;
y
E
o
cos(&ohgr;
t
+&pgr;/2).
Thus, the LHCP signal is 180 degrees out of phase with the RHCP signal, which gives at least a 3.0 dB signal loss in practice. If the receiver is sensitive, this may not be a problem. However, for many applications, it is desirable to reduce the amount of receiver sensitivity needed so as to enhance the signal-to-noise ratio. Further, a less sensitive receiver is less expensive to manufacture. Also, many applications utilizing GPS technology simply cannot physically locate the receiving antenna such that a direct line-of-sight with the satellite transmitting the RHCP signal is possible.
Since some applications utilizing GPS technology must position the receiving antenna such that signal reflection is necessary, an antenna is needed which can make the best use of a reflected signal. In addition, a method of using the antenna to best make use of such a reflected RHCP signal is needed.
SUMMARY OF THE INVENTION
An antenna system, comprising a left-hand circular polarized antenna, is disclosed for use in receiving signals from a GPS location satellite which are originally-transmitted as RHCP signals. Reception occurs after the right-hand circular polarized signal is reflected, or bounces off of, a surface one or more times. The number of reflections must be an odd number. The left-hand circular polarized antenna may be mounted underneath a vehicle or a building overhang. The method of the invention comprises the steps of transmitting a right-hand circular polarized signal and receiving the signal using a left-hand circular polarized antenna placed in a location where the right-hand circular polarized signal must be reflected by an odd number of surfaces before reception.


REFERENCES:
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patent: 4845506 (1989-07-01), Shibata et al.
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patent: 4893129 (1990-01-01), Kodera et al.
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patent: 4968984 (1990-11-01), Katoh et al.
patent: 5003318 (1991-03-01), Berneking et al.
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patent: 5212494 (1993-05-01), Hofer et al.
patent: 5298908 (1994-03-01), Piele
patent: 5995044 (1999-11-01), Kunysz et al.
Author: Unknown, Date: Unknown, Antenna Systems for Space Communications, “Circular Polarization”, Ch. 19, pp. 19-9, 19-10.
Amateur Radio Relay League, 1997, ARRL Handbook for Radio Amateurs, “Repeaters, Satellites, EME and Direction Finding”, Ch. 23, pp. 23.36, 23.37.

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