Very small aperture terminal & antenna for use therein

• US 5,745,084 A
• Filed: 10/13/1995
• Issued: 04/28/1998
• Est. Priority Date: 06/17/1994
• Status: Expired due to Term

• Current Assignee: Datasec Corporation
• Original Assignee: Bruce B. Lusignan
• Inventors: Lusignan, Bruce B.
• Primary Examiner(s): Le, Hoanganh T.
• Application Number:
  US08/542,493
• Time in Patent Office: 928 Days
• Field of Search: 343/781 P, 343/DIG. 2, 343/781 R, 343/781 CA, 343/782, 343/783
• US Class Current: 343/781.00P
• CPC Class Codes: H01Q 13/02 Waveguide horns
• CPC Class Codes: H01Q 19/12 wherein the surfaces are concave H01Q19/18 takes precedence
• CPC Class Codes: H01Q 19/13 the primary radiating source being a single radiating element, e.g. a dipole, a slot, a waveguide termination H01Q19/15 takes precedence
• CPC Class Codes: H01Q 19/132 Horn reflector antennas; Off-set feeding
• CPC Class Codes: H01Q 19/193 with feed supported subreflector splash plate feeds H01Q19/134
• CPC Class Codes: H01Q 21/24 Combinations of antenna units polarised in different directions for transmitting or receiving circularly and elliptically polarised waves or waves linearly polarised in any direction circularly polarised patch antennas H01Q9/0428; circularly polarised horns H01Q13/0241; cross-polarised horns H01Q13/0258; polarisation converters H01Q15/242; cross-polarised rear feeds H01Q19/136; crossed polarisation dual antenna H01Q25/001
• CPC Class Codes: H01Q 21/28 Combinations of substantially independent non-interacting antenna units or systems multiple beam H01Q25/00
• CPC Class Codes: H01Q 25/00 Antennas or antenna systems providing at least two radiating patterns arrangements for changing or varying the orientation or the shape of the directional pattern H01Q3/00
• CPC Class Codes: H01Q 3/22 varying the orientation in accordance with variation of frequency of radiated wave
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence
• CPC Class Codes: H01Q 5/45 using two or more feeds in association with a common reflecting, diffracting or refracting device
• CPC Class Codes: H01Q 5/55 for horn or waveguide antennas
• CPC Class Codes: H04B 7/18517 Transmission equipment in earth stations
• CPC Class Codes: H04B 7/18578 Satellite systems for providing broadband data service to individual earth stations for selecting H04W; provisions for broadband connection, H04Q11/0478
• CPC Class Codes: H04B 7/18597 Arrangements for system physical machines management, i.e. for construction, operations control, administration, maintenance
• CPC Class Codes: Y10S 343/02 Satellite-mounted antenna

Abstract

A data transmitting/receiving satellite terminal for transmitting to and receiving from a geosynchronous satellite employs an antenna having nulls in its antenna receiving pattern at a first frequency corresponding to satellites spaced at regular intervals from the satellite. In addition, a phase and amplitude compensation network adjusts a phase and amplitude of the transmitted signal to compensate for transmitting at a different frequency than for which the antenna is optimally designed. The antenna includes a main parabolic reflector, and two side parabolic reflectors offset from a plane parallel to the main parabolic reflector. Each of the reflectors uses a dual frequency feed horn to couple energy to and from the reflector to a dipole exciter to which the receiving electronics is coupled. The above terminal is particularly useful in C-Band applications.

Claims

1. A data transmitting/receiving satellite terminal for transmitting to and receiving from a geosynchronous satellite comprising:

a) an antenna having an aperture forming an antenna receiving pattern with nulls at a first frequency, said nulls corresponding to satellites spaced at regular intervals from the satellite; and

b) a phase and amplitude compensation network coupled to said antenna, said compensation network adjusting a phase and amplitude of a transmitted signal to compensate for transmitting at a second frequency different than the first frequency, wherein the antenna aperture further comprises a main parabolic reflector and two side parabolic reflectors.

2. The satellite terminal according to claim 1, wherein the phase and amplitude compensation network compensates each signal being sent to each of the reflectors satisfying the following relationship:

space="preserve" listing-type="equation">Total Power=W(1+0.295+0.295)

where W=the power to the main reflector in Watts, and 0.295 represents the approximate power of each signal being sent to the side reflectors, and the phases of the signals being sent to the one side reflector, to the main reflector and to the other side reflector are all equal.

3. The satellite terminal according to claim 2, wherein the phase and amplitude compensation network compensates for the difference in frequency by modifying the power and phase of each signal being radiated from the main reflector and the two side reflectors so that nulls in the transmit pattern of the antenna at the transmit frequency match the satellite orbital configuration.

4. The satellite terminal according to claim 1, wherein the phase and amplitude compensation network compensates for the difference in frequency by modifying the power and phase of each signal being radiated from the main reflector and the two side reflectors so that nulls in the transmit pattern of the antenna at the transmit frequency match the satellite orbital configuration.

5. An apparatus for sending signals to and receiving signals from a satellite, comprising:

a) means for creating nulls in a receiving antenna pattern matched to satellites spaced from the satellite at regular intervals, which receiving antenna pattern is defined at a first frequency; and

b) means for compensating for a transmitting antenna pattern by adjusting a phase and amplitude of a transmitted signal, which transmitting antenna pattern is defined at a second frequency, wherein the means for creating nulls comprises a main parabolic reflector, and two side parabolic reflectors.

6. The apparatus according to claim 5, wherein the means for compensating comprises a coupling network which adjusts the phase and amplitude of the transmitted signal for each of three apertures of the means for creating nulls.

7. The satellite terminal according to claim 6, wherein the means for compensating compensates for the difference in frequency by modifying the power and phase of each signal being radiated from the main reflector and the two side reflectors so that nulls in the transmit pattern of the antenna at the transmit frequency match the satellite orbital configuration.

8. The satellite terminal according to claim 5, wherein the means for compensating compensates for the difference in frequency by modifying the power and phase of each signal being radiated from the main reflector and the two side reflectors so that nulls in the transmit pattern of the antenna at the transmit frequency match the satellite orbital configuration.

9. A data transceiver for transmitting to and receiving from within a satellite system, which includes a desired satellite and a plurality of interfering satellites, comprising:

an antenna having an aperture shaped to create an antenna receiving pattern including a main lobe having gain for the received signal at a first frequency from the desired satellite and a null for each of at least four of the plurality of interfering satellites; and

a phase and amplitude compensation network coupled to said antenna, said compensation network adjusting a phase and amplitude of a transmitted signal to compensate for transmitting at a frequency different than the first frequency, wherein the aperture has at least three primary areas, and wherein said compensation network adjusts the phase and amplitude of a transmitted signal to each of the three primary areas of said antenna.

10. A data transceiver for receiving at a first frequency from and transmitting at a second frequency to a first satellite having at least four adjacent satellites, comprising:

an antenna shaped to form an antenna receiving pattern including a main lobe having a null for each of the four adjacent satellites; and

a phase and amplitude compensation network connected to said antenna, said compensation network adjusting the phase and amplitude of a transmitted signal to form an antenna transmitting pattern including a main lobe having a null for each of the four adjacent satellites, wherein said antenna includes three primary areas, and wherein said compensation network adjusts the phase and amplitude of a transmitted signal to each of the three primary areas of said antenna.

11. The data transceiver of claim 10, wherein said three primary areas comprise a center primary antenna area and two outer primary antenna areas, and said compensation network adjusts each signal to each of the three primary areas of said antenna satisfying the following relationship:

space="preserve" listing-type="equation">Total Power=W(1+0.3+0.3)

where W=the power to the center primary antenna area in Watts, and 0.3 represents the approximate power of each signal being sent to the two outer primary antenna areas, and the phases of the signals being sent to each primary antenna area are all equal.

12. A data transceiver for receiving at a first frequency from and transmitting at a second frequency to a first satellite having at least four adjacent satellites, comprising:

an antenna shaped to form an antenna receiving pattern including a main lobe having a null for each of the four adjacent satellites; and

a phase and amplitude compensation network coupled to said antenna, said compensation network adjusting the phase and amplitude of a transmitted signal to form an antenna transmitting pattern including a main lobe having a null for each of the four adjacent satellites, wherein said antenna is shaped to include a main parabolic reflector and two side parabolic reflectors, and wherein said compensation network adjusts the phase and amplitude of a transmitted signal to the main parabolic reflector and two side parabolic reflectors.

13. The data transceiver of claim 12, wherein said compensation network adjusts each signal to the main reflector and the two side reflectors satisfying the following relationship:

space="preserve" listing-type="equation">Total Power=W(1+0.29+0.29)

where W=the power to the main parabolic reflector in Watts, and 0.29 represents the approximate power of each signal being sent to each side parabolic reflector, and the phases of the signals being sent to the main parabolic reflector and two side parabolic reflectors are all equal.