1. Field of the Invention
The present invention relates generally to a microstrip antenna for use on a missile or the like. More specifically, the present invention relates to a microstrip antenna which trnsmits telemetry data and which is adapted for use on small diameter projectiles such as a missile.
2. Description of the Prior Art
A microstrip antenna operates by resonating at a frequency. The conventional design for a microstrip antenna utilizes printed circuit board techniques mounting a copper patch on the top layer of a dielectric with a ground plane on the bottom of the dielectric. The frequency at which the antenna operates is approximately a half wavelength in the microstrip medium of dielectric below the copper patch and air above the copper patch.
However, there is a need to isolate the microstrip antenna from radio frequency signals at different frequencies than the operating frequency for the antenna.
To achieve isolation, prior art microstrip antenna designs have used an external filter. This external component requires extra space, which is generally not available on weapons systems, such as small diameter projectiles, and also require interconnecting coaxial cables, which are expensive and not practical when there are severe limitations on available apace in weapons systems.
Accordingly, there is a need for a microstrip antenna which operates in the TM frequency band, requires minimal space, and provides for isolation, protection and amplification. More specifically, there is a need for a TM frequency band microstrip antenna which generates an omni-directional antenna pattern, and provides for a 50 dB isolation from a frequency in the GPS L1 frequency band.
The present invention overcomes some of the disadvantages of the past including those mentioned above in that it comprises a highly effective and efficient microstrip antenna designed to transmit telemetry data from an approximately nine inch diameter projectile. The microstrip antenna comprising the present invention is configured to wrap around the projectile's body without interfering with the aerodynamic design of the projectile.
The TM Band microstrip antenna operates at 2.25 GHz with a bandwidth of ±10 MHz. Eight microstrip antenna elements equally spaced around the projectile provide for linear polarization and a quasi-omni directional radiation pattern. Each of the eight microstrip antenna elements include a tuning stub on top edge of the element to allow for fine tuning of the element to the operating frequency.
There is a gap around each of the eight antenna elements with the remainder of the antenna covered with copper. The antenna element's electric field is confined generally to the gap. The antenna's feed network consist of equal amplitude and phase power dividers and filters.
The feed network has two identical filters with each filter comprising a band stop filter. The band stop filter is tuned at the GPS L1 frequency so that noise from the TM transmitting antenna elements at the GPS frequency will not increase the noise floor of near-by GPS antenna receiving elements.
Referring to
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At this time, it should be noted that the circuit board 28 and a ground board 38 which is positioned below the circuit board 28 are each fabricated from a dielectric. The dielectric used in the preferred embodiment is Duroid 6002 commercially available from Rogers Corporation of Rogers, Conn. The top layer and bottom layer of the circuit board and the bottom layer of the ground board respectively have a one ounce copper plating 46, 48 and 50 with a 0.0014 inch thickness that is etched off to provide the antenna element, feed network and ground patterns illustrated in
There is also a four sided gap 40 formed around each side 34, 36, 42 and 44 of the eight antenna elements 12, 14, 16, 18, 20, 22, 24 and 26 of microstrip antenna 10. The four sided gap 40 exposes the top surface of the dielectric 28. The TM microstrip antenna's electric field is confined primarily to the four sided gap 40 around each of the antenna elements which is substantial different than a conventional microstrip copper antenna element where the electric field extends well beyond the antenna element.
Referring to
The feed network 53 also includes a plurality of branch transmission lines 58, fabricated from etched copper, which connect the main transmission line 55 to the eight antenna elements 12, 14, 16, 18, 20, 22, 24, and 26.
Each antenna element 12, 14, 16, 18, 20, 22, 24 and 28 is capcitively coupled to one of the branch transmission lines 58 of feed network 53 by a probe 60 which is also an etched copper transmission line. The probes 60 are positioned directly underneath each antenna element 12, 14, 16, 18, 20, 22, 24, and 26 and terminate below each antenna element 12, 14, 16, 18, 20, 22, 24 and 26. Capacitive coupling of the RF signals to the eight antenna elements 12, 14, 16, 18, 20, 22, 24 and 26 from their associated probes 60 and 62 is through the dielectric layer 28.
The main feed line 53, branch feed lines 58 and probes 60 are configured such that feed network 53 operates as equal amplitude, equal phase power dividers.
Referring to
Band stop filter 76 includes 3 open circuit transmission lines 83, 84 and 86 and two interconnecting transmission lines 88 and 90 which form the five sections of band stop filter 76. Band stop filter 78 is identical to band stop filter 76 in that it is a five section band stop filter. Each filter 76 and 78 is connected to the main transmission line 55 for feed network 53.
Each band stop filter 76 and 78 is tuned at the GPS L1 frequency which is approximately 1.575 GHz. When filters 76 and 78 are tuned at the GPS frequency, noise from the TM transmitting antenna elements at the GPS frequency will not increase the noise floor of near-by GPS antenna receiving elements. A minimum isolation of 50 dB is required and achieved by utilizing the 50 Band stop filters 76 and 78 in the preferred embodiment.
Referring to
From the foregoing, it is readily apparent that the present invention comprises a new, unique, and exceedingly useful TM microstrip antenna adapted for use on small diameter projectiles, which constitutes a considerable improvement over the known prior art. Many modifications and variations of the present invention are possible in light of the above teachings. It is to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
This application is a continuation-in-part of U.S. patent application Ser. No. 10/664,614, filed Sep. 19, 2003.
Number | Date | Country | |
---|---|---|---|
Parent | 10664614 | Sep 2003 | US |
Child | 10817412 | Mar 2004 | US |