1. Field of the Invention
The present invention relates generally to a microstrip antenna for use on a weapons system. More specifically, the present invention relates to a TM microstrip antenna with frequency coverage over a frequency range of 2200 to 2300 MHz which is the TM frequency band as well as coverage over the L1 GPS frequency band.
2. Description of the Prior Art
The Hardened Subminiature Telemetry and Sensor System (HSTSS) program is a Department of Defense for identifying, developing and validating inexpensive, rugged, microelectronic technologies for incorporation into instrumentation and telemetry systems. The instrumentation and telemetry systems incorporating HSTSS technology are designed for use in the harsh environments of small missile and gun launched munitions applications. HSTSS qualification of new technologies and state of the art components will result in inexpensive and reliable components for the successful development, fielding and maintenance of modern weapons systems.
There is a need for a small diameter, lightweight TM microstrip antenna with GPS frequency coverage which meets the requirements of HSTSS program. The major problems associated with using current technology are the limitation on size requirements for an antenna with GPS and TM operational capability, and the requirement for a 40 dB minimum isolation between the GPS and TM antenna elements.
The present invention overcomes some of the disadvantages of the prior art in that it comprises a highly effective TM microstrip antenna with frequency coverage over a frequency range of 2200 to 2300 MHz which is the TM frequency band as well as coverage over the L1 GPS frequency band.
The TM antenna radiating element is a copper radiating element mounted on the top layer of a circuit board for the antenna. A ceramic GPS square shaped microstrip antenna is positioned above the TM antenna radiating element on the circuit board. A filter top printed circuit board is also included within the TM microstrip antenna. The filter top printed circuit board has a first filter which is a band stop filter at the TM frequency of approximately 2.25 GHz, and a second filter which is a band stop filter at the GPS frequency of approximately 1575 MHz.
The Antenna is fabricated from high dielectric constant material (10.2) to reduce the size of the antenna which has a diameter of 1.364 inches. Forty dB isolation is achieved in the TM and GPS frequency bands by the band stop filters on the filter top printed circuit board.
Referring to
As shown in
The dielectric substrate 20 has the shape of a circle with a diameter of about 1⅜ inches. Positioned around the circumference of dielectric substrate 20 are eight equally spaced apart 0.089-inch diameter mounting holes 24 which are adapted for mounting the antenna 12 to a projectile.
The radiating element 10 for antenna 12 is also circular in shape and is adapted to transmit an RF (radio frequency) signal within the S-band frequency range of 2.2–2.3 GHz. The diameter of radiating element is approximately ⅞ of an inch. Radiating element 10 includes a first pair of tuning tabs 26 and 28 which are positioned 180° from one another about the circumference of radiating element 10. Radiating element 10 also includes a second pair of tuning tabs 30 and 32 which are positioned 180° from one another about the circumference of radiating element 10. The angle between adjacent tuning tabs 28 and 30 is approximately 80° as is best indicated by arrow 34.
The upper surface of dielectric substrate 20 also has an isolated feed 36. The feed 36, which is a 50 ohm input and is electrically connected to filter 14, passes through dielectric substrate 20 to the filter 14.
Referring now to
Antenna 12 is designed to operate in the S-band frequency range of 2.2–2.3 GHz, but has the capability to operate at frequencies of 2.37 GHz. The polarization of antenna 12 has two modes resulting from the two feeds 16 and 18 to radiating element 10 of antenna 12.
The telemetry antenna of the present invention is identical to the telemetry antenna of U.S. Pat. No. 6,630,907, which issued Oct. 7, 2003 to Marvin L. Ryken and Albert F. Davis, co-inventors of the present invention.
Referring to
Referring to
Filter Top Printed Circuit Board 58 includes two-quarter wavelength open stubs 60 and 62 separated by a quarter wavelength copper transmission line 64 which form a band stop filter 66 at the TM frequency of approximately 2.25 GHz. The feed wire from the GPS antenna is connected to band stop filter 66 on the Filter Top Printed Circuit Board 58 shown in
Filter Top Printed Circuit Board 58 of
Referring to
Referring to
The telemetry antenna 12 when assembled has four printed circuit boards stacked on top of one another. The Boards comprising antenna 12 are the Circuit Board 20, the Ground Board 54, the Filter Top Printed Circuit Board 58 and the Filter Bottom Printed Circuit Board 88. The Circuit PC and Ground PC Boards are fabricated from Rogers Corporation's Duriod 6010 with a 0.050-inch thickness clad with one-ounce copper. The Filter Top and Bottom PC Boards are fabricated from Rogers Corporation's Duriod 6002 with a 0.020-inch thickness clad with one-ounce copper. All the Boards of telemetry antenna 12 are gold plated so that resistance is minimized for maximum isolation and for environmental protection.
The assembly process for antenna 12 is as follows. The GPS antenna 50 is epoxied to the circuit board 20 in the manner illustrated in
Filters 66 and 68 are then connected to the Circuit and Ground Printed Circuit Boards 20 and 54, respectively, to form the final antenna. The TM antenna radiating element 10 and the GPS antenna 50 are each circular polarized and require tuning in both the horizontal and vertical polarization modes to achieve the required results. The GPS antenna 50 has a very narrow frequency bandwidth and the VSWR 100 (Voltage Standing Wave Ratio) over the L1 frequency band is illustrated in
Referring to
From the foregoing, it is readily apparent that the present invention comprises a new, unique, and exceedingly useful TM microstrip antenna with GPS frequency coverage for use with a projectile or the like, 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.
Number | Name | Date | Kind |
---|---|---|---|
5068669 | Koert et al. | Nov 1991 | A |
5410322 | Sonoda | Apr 1995 | A |
6281844 | Kodim et al. | Aug 2001 | B1 |
6326923 | Shigihara | Dec 2001 | B2 |
6549168 | Ryken et al. | Apr 2003 | B1 |
6630907 | Ryken et al. | Oct 2003 | B1 |