Dual-band antenna systems
View Patent ↗Dual-band antenna systems and methods of fabricating and using the same are provided. A tunable dual-polarization (left-hand circular polarized (LHCP) and right-hand circular polarized (RHCP)) antenna can be used both for L-band (1.215 gigahertz (GHz)-1.85 GHz) and Ka-band (32.3 GHz-34.2 GHz) operation. The antenna system can be an embedded antenna system, which can be used for 3U CubeSats, with full polarization diversity able to operate in two widely spaced frequency bands (L-band and Ka-band) of the spectrum. The antenna system can include three layers, including a top substrate, a bottom substrate, and a ground plane disposed between the top substrate and the bottom substrate.
1. An antenna system, comprising:
a top substrate;
a bottom substrate;
a ground plane disposed between the top substrate and the bottom substrate;
a first array of first antenna elements disposed on the top substrate and configured to operate in the L-band;
a second array of second antenna elements disposed on the top substrate and configured to operate in the Ka-band;
a first feed network disposed on the bottom substrate and electrically connected to the first array; and
a second feed network disposed on the bottom substrate and electrically connected to the second array,
the first feed network comprising a plurality of first output feedlines respectively connected to the first antenna elements,
the second feed network comprising a plurality of second output feedlines respectively connected to the second antenna elements,
each first output feedline comprising two diodes,
each second output feedline comprising two diodes, and
the antenna system further comprising:
a plurality of first via pairs respectively connecting the first antenna elements to the first output feedlines; and
a plurality of second via pairs respectively connecting the second antenna elements to the second output feedlines,
the two diodes of each first output feedline being in direct physical contact with two vias, respectively, of one of the first via pairs, and
the two diodes of each second output feedline being in direct physical contact with two vias, respectively, of one of the second via pairs.
2. The antenna system according to claim 1 , further comprising:
a plurality of first via pairs respectively connecting the first antenna elements to the first output feedlines; and
a plurality of second via pairs respectively connecting the second antenna elements to the second output feedlines.
3. The antenna system according to claim 1 , the first feed network comprising a first feed connection line extending to a first portion of an outer perimeter of the bottom substrate, and
the second feed network comprising a second feed connection line extending to a second portion of the outer perimeter of the bottom substrate.
4. The antenna system according to claim 1 , the first array comprising eight first antenna elements disposed in a 2×4 arrangement.
5. The antenna system according to claim 4 , the second array comprising sixteen second antenna elements disposed in a 1×16 arrangement.
6. The antenna system according to claim 1 , the second array comprising sixteen second antenna elements disposed in a 1×16 arrangement.
7. The antenna system according to claim 1 , each first antenna element being a patch antenna element, and
each second antenna element being a patch element.
8. The antenna system according to claim 1 , each first antenna element being a patch antenna element with two opposite corners each being truncated, and
each second antenna element being a patch element with two opposite corners each being truncated.
9. The antenna system according to claim 1 , each first antenna element having an upper surface with an area that is at least 2 times larger than an area of an upper surface of each second antenna element.
10. The antenna system according to claim 1 , each first antenna element having an upper surface with an area that is at least 3 times larger than an area of an upper surface of each second antenna element.
11. The antenna system according to claim 1 , each first antenna element having an upper surface with an area that is at least 4 times larger than an area of an upper surface of each second antenna element.
12. The antenna system according to claim 1 , the first feed network being a microstrip transmission line-based network, and the second feed network being a microstrip transmission line-based network.
13. The antenna system according to claim 1 , each first antenna element being configured to operate as both left-hand circular polarized (LHCP) and right-hand circular polarized (RHCP), and
each second antenna element being configured to operate as both LHCP and RHCP.
14. The antenna system according to claim 1 , the antenna system configured to operate the first antenna array and the second antenna array simultaneously.
15. A 3 U CubeSat, comprising:
a base; and
the antenna system according to claim 1 disposed on the base,
the antenna system and the base each having a length of about 30 centimeters (cm) and a width of about 10 cm, and
the 3 U CubeSat having a height of about 10 cm.
16. An antenna system, comprising:
a top substrate;
a bottom substrate;
a ground plane disposed between the top substrate and the bottom substrate;
a first array of first antenna elements disposed on the top substrate and configured to operate in the L-band;
a second array of second antenna elements disposed on the top substrate and configured to operate in the Ka-band;
a first feed network disposed on the bottom substrate and electrically connected to the first array; and
a second feed network disposed on the bottom substrate and electrically connected to the second array,
the first feed network comprising a plurality of first output feedlines respectively connected to the first antenna elements,
the second feed network comprising a plurality of second output feedlines respectively connected to the second antenna elements,
the antenna system further comprising:
a plurality of first via pairs respectively connecting the first antenna elements to the first output feedlines; and
a plurality of second via pairs respectively connecting the second antenna elements to the second output feedlines,
each first output feedline comprising two diodes,
each second output feedline comprising two diodes,
the two diodes of each first output feedline being in direct physical contact with two vias, respectively, of one of the first via pairs,
the two diodes of each second output feedline being in direct physical contact with two vias, respectively, of one of the second via pairs,
the first feed network comprising a first feed connection line extending to a first portion of an outer perimeter of the bottom substrate,
the second feed network comprising a second feed connection line extending to a second portion of the outer perimeter of the bottom substrate,
the first array comprising eight first antenna elements disposed in a 2×4 arrangement,
the second array comprising sixteen second antenna elements disposed in a 1×16 arrangement,
each first antenna element being a patch antenna element with two opposite corners each being truncated,
each second antenna element being a patch element with two opposite corners each being truncated,
each first antenna element having an upper surface with an area that is at least 4 times larger than an area of an upper surface of each second antenna element,
the first feed network being a microstrip transmission line-based network,
the second feed network being a microstrip transmission line-based network,
each first antenna element being configured to operate as both left-hand circular polarized (LHCP) and right-hand circular polarized (RHCP),
each second antenna element being configured to operate as both LHCP and RHCP, and
the antenna system configured to operate the first antenna array and the second antenna array simultaneously.
17. A 3 U CubeSat, comprising:
a base; and
the antenna system according to claim 16 disposed on the base,
the antenna system and the base each having a length of about 30 centimeters (cm) and a width of about 10 cm, and
the 3 U CubeSat having a height of about 10 cm.