Solar powered satellite system
First Claim
1. A power control system, comprising:
- a first interface configured to be coupled to a satellite receiver and configured to receive a power signal from the satellite receiver;
a voltage converter electrically coupled to the first interface, the voltage converter configured to adjust a voltage of the power signal received from the satellite receiver to a predetermined voltage;
a second interface configured to be coupled to a solar panel assembly and configured to receive a power signal from the solar panel assembly;
a third interface configured to be coupled to at least one power consumer of a satellite antenna system;
a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal by electrically coupling the second interface to the third interface when the voltage of the power signal from the solar panel assembly is greater than the predetermined voltage and further configured to electrically couple the first interface to the third interface when the voltage of the power signal from the solar panel assembly is less than the predetermined voltage;
a first bias-T electrically coupled between the first interface, the voltage converter and the third interface, the first bias-T configured to;
receive the power signal received from the satellite receiver and control and RF signals from the satellite receiver along a first single bus;
split the power signal received from the satellite receiver from the control and RF signals from the satellite receiver;
transmit the power signal received from the satellite receiver to the voltage converter; and
transmit the control and RF signals received from the satellite receiver to the third interface; and
a second bias-T electrically coupled between the first bias-T, the source selection circuit and the third interface, the second bias-T configured to;
receive the selected power signal from the source selection circuit;
receive the control and RF signals from the first bias-T;
combine the selected power signal received from the source selection circuit with the control and RF signals from the first bias-T; and
transmit the combined selected power signal and the control and RF signals to the third interface along a second single bus.
3 Assignments
0 Petitions
Accused Products
Abstract
A solar powered satellite system is provided. A power control system, for example, of the solar powered satellite system may include, but is not limited to, a first interface configured to receive a power signal from the satellite receiver, a voltage converter electrically coupled to the first interface, the voltage converter configured to reduce a voltage of the power signal received from the satellite receiver to a predetermined voltage, a second interface configured to receive a power signal from the solar panel assembly, a third interface configured to be coupled to at least one power consumer of a satellite antenna system, and a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal based upon a comparison between the predetermined voltage and a voltage of the power signal from the solar panel assembly.
15 Citations
14 Claims
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1. A power control system, comprising:
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a first interface configured to be coupled to a satellite receiver and configured to receive a power signal from the satellite receiver; a voltage converter electrically coupled to the first interface, the voltage converter configured to adjust a voltage of the power signal received from the satellite receiver to a predetermined voltage; a second interface configured to be coupled to a solar panel assembly and configured to receive a power signal from the solar panel assembly; a third interface configured to be coupled to at least one power consumer of a satellite antenna system; a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal by electrically coupling the second interface to the third interface when the voltage of the power signal from the solar panel assembly is greater than the predetermined voltage and further configured to electrically couple the first interface to the third interface when the voltage of the power signal from the solar panel assembly is less than the predetermined voltage; a first bias-T electrically coupled between the first interface, the voltage converter and the third interface, the first bias-T configured to; receive the power signal received from the satellite receiver and control and RF signals from the satellite receiver along a first single bus; split the power signal received from the satellite receiver from the control and RF signals from the satellite receiver; transmit the power signal received from the satellite receiver to the voltage converter; and transmit the control and RF signals received from the satellite receiver to the third interface; and a second bias-T electrically coupled between the first bias-T, the source selection circuit and the third interface, the second bias-T configured to; receive the selected power signal from the source selection circuit; receive the control and RF signals from the first bias-T; combine the selected power signal received from the source selection circuit with the control and RF signals from the first bias-T; and transmit the combined selected power signal and the control and RF signals to the third interface along a second single bus. - View Dependent Claims (2, 3, 4, 5)
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6. A method of controlling a power control system, comprising:
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receiving, from a solar panel assembly by the power control system, a first power signal; receiving, from a satellite receiver by the power control system, a second power signal and RF signals from a first single bus; splitting, by a first bias-T circuit the second power signal from the control and RF signals, the second power signal being transmitted to a voltage converter by the first bias-T circuit and the RF control signal being transmitted to a second bias-T circuit by the first bias-T circuit; reducing, by the voltage converter, a voltage of the second power signal received from the satellite receiver to a predetermined voltage; selecting, by a source selection circuit, one of the first power signal and the reduced voltage of the second power signal as a power source for a power consumer of a satellite antenna system based upon a comparison between the first power signal and the predetermined voltage; combining, by the second bias-T circuit, the selected power source for the power consumer of the satellite antenna system with the RF control signal; and electrically coupling, by the second bias-T circuit, the selected power source and the RF control signal to the power consumer of the satellite antenna system via a second single bus. - View Dependent Claims (7, 8)
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9. A solar power satellite system, comprising:
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a satellite antenna system coupled to at least one power consumer; a satellite receiver configured to output a first power signal; a solar panel assembly comprising at least one solar panel configured to output a second power signal; and a power control system, comprising; a first interface configured to be coupled to the satellite receiver and configured to receive the first power signal; a voltage converter electrically coupled to the first interface, the voltage converter configured to reduce a voltage of the first power signal to a predetermined voltage; a second interface configured to be coupled to the solar panel assembly and configured to receive the second power signal; a third interface configured to be coupled to the at least one power consumer of the satellite antenna system; a source selection circuit electrically coupled to the voltage converter, the solar panel assembly and the third interface, the source selection circuit configured to output a selected power signal by electrically couple the second interface to the third interface when the voltage of the second power signal from the solar panel assembly is greater than the predetermined voltage and further configured to electrically couple the first interface to the third interface when the voltage of the second power signal from the solar panel assembly is less than the predetermined voltage; a first bias-T electrically coupled between the first interface, the voltage converter and the third interface, the first bias-T configured to; receive the first power signal received from the satellite receiver and control and RF signals from the satellite receiver along a single bus; split the first power signal received from the satellite receiver from the control and RF signals from the satellite receiver; transmit the first power signal received from the satellite receiver to the voltage converter; and transmit the control and RF signals received from the satellite receiver to the third interface; and a second bias-T electrically coupled between the first bias-T, the source selection circuit and the third interface, the second bias-T configured to; receive the selected power signal from the source selection circuit; receive the control and RF signals from the first bias-T; combine the selected power signal received from the source selection circuit with the control and RF signals from the first bias-T; and transmit the combined selected power signal and the control and RF signals to the third interface along a single bus. - View Dependent Claims (10, 11, 12, 13, 14)
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Specification