초록 ▼

The present invention is directed to a fuze application capable of GPS (Global Positioning System) and proximity radar functionality by co-locating a proximity radar antenna with a GPS DRA (Dielectric Resonator Antenna) fuze. The GPS DRA fuze has a HE11δ mode structure resulting in an E-field n

The present invention is directed to a fuze application capable of GPS (Global Positioning System) and proximity radar functionality by co-locating a proximity radar antenna with a GPS DRA (Dielectric Resonator Antenna) fuze. The GPS DRA fuze has a HE11δ mode structure resulting in an E-field null at the center. The monopole proximity radar antenna is mounted in the E-field null center and is thus electrically isolated from the GPS DRA fuze. The high dielectric constant permits the GPS DRA fuze to operate in the L1 frequency and the electrically shortened proximity radar antenna to resonate in the C-Band within a small form factor. The GPS DRA fuze maintains a forward-looking CP (circular polarization) pattern while proximity antenna maintains a desirable monopole pattern. Nesting allows mounting of both GPS and proximity radar antennas on the fuze nose while reducing the total space occupied.

대표청구항 ▼

What is claimed is: 1. An antenna system, comprising: a proximity radar antenna; and a GPS (Global Positioning System) DRA (Dielectric Resonator Antenna); wherein the proximity radar antenna is located within the GPS DRA and is electrically isolated from the GPS DRA. 2. The antenna system as cla

What is claimed is: 1. An antenna system, comprising: a proximity radar antenna; and a GPS (Global Positioning System) DRA (Dielectric Resonator Antenna); wherein the proximity radar antenna is located within the GPS DRA and is electrically isolated from the GPS DRA. 2. The antenna system as claimed in claim 1, wherein the GPS DRA comprises: at least one feed probe; and a DRA cone; wherein the feed probe is mounted within the DRA cone. 3. The antenna system as claimed in claim 2, wherein the DRA cone comprises a dielectric cone. 4. The antenna system as claimed in claim 3, wherein the dielectric cone comprises a dielectric material with a dielectric constant of ε≈25. 5. The antenna system as claimed in claim 3, wherein the GPS DRA has a HE11δ mode structure driven by the feed probe and an E-field null exists at the center of the dielectric cone. 6. The antenna system as claimed in claim 5, wherein the proximity radar antenna is mounted in the center of the dielectric cone. 7. The antenna system as claimed in claim 6, wherein the proximity radar antenna is a monopole and the GPS DRA comprises two feed probes. 8. The antenna system as claimed in claim 6, wherein the proximity radar antenna and the GPS DRA are electrically isolated from each other. 9. The antenna system as claimed in claim 6, wherein the proximity radar antenna is electrically shortened. 10. The antenna system as claimed in claim 9, wherein the proximity radar antenna resonates in the C-Band. 11. The antenna system as claimed in claim 10, wherein the GPS DRA cone is a component of a fuze nose, the form factor of the fuze nose is approximately 30 millimeters by 30 millimeters, and the height of the proximity radar antenna and feed probe is no greater than approximately 30 millimeters. 12. A method of providing an antenna system, comprising the steps of: providing a proximity radar antenna; providing a GPS (Global Positioning System) DRA (Dielectric Resonator Antenna); and mounting the proximity radar antenna within the GPS DRA such that the proximity radar antenna is electrically isolated from the GPS DRA. 13. The method of claim 12, wherein the GPS DRA comprises: at least one feed probe; and a DRA cone; wherein the feed probe is mounted within the DRA cone. 14. The method of claim 13, wherein the DRA cone comprises a dielectric cone. 15. The method of claim 14, wherein the dielectric cone comprises a dielectric material with a dielectric constant of ε≈25. 16. The method of claim 14, wherein the GPS DRA has a HE11δ mode structure driven by the feed probe and an E-field null exists at the center of the dielectric cone. 17. The method of claim 16, wherein the proximity radar antenna is mounted in the center of the dielectric cone. 18. The method of claim 17, wherein the proximity radar antenna is a monopole and the GPS DRA comprises two feed probes. 19. The method of claim 17, wherein the proximity radar antenna and the GPS DRA are electrically isolated from each other. 20. The method of claim 17, wherein the proximity radar antenna is electrically shortened. 21. The method of claim 20, wherein the proximity radar antenna resonates in the C-Band. 22. The method of claim 21, wherein the GPS DRA cone is a component of a fuze nose, the form factor of the fuze nose is approximately 30 millimeters by 30 millimeters, and the height of the proximity radar antenna and feed probe is no greater than approximately 30 millimeters. 23. A system for fuzing, comprising: a GPS (Global Positioning System) DRA (Dielectric Resonator Antenna), comprising: a dielectric DRA cone which has a form factor of approximately 30 millimeters by 30 millimeters and is comprised of a dielectric material with a dielectric constant of ε≈25; and one or more feed probes, which have a height of no greater than approximately 30 millimeters, mounted within the dielectric DRA cone; wherein the GPS DRA has a HE11δ mode structure driven by the feed probes and an E-field null exists at the center of the dielectric cone; an electrically shorted monopole proximity radar antenna which has a height of no greater than approximately 30 millimeters and resonates in the C-Band; wherein the GPS DRA and the electrically shortened monopole proximity radar antenna are components of a fuze nose, the electrically shortened monopole proximity radar antenna is mounted in the center of the dielectric cone of the GPS DRA, and the electrically shortened monopole proximity radar antenna is electrically isolated from the GPS DRA.