Battery regulated bus spacecraft power control system
AssigneeTRW Inc.
InventorsDarwin K. Decker, Charles B. Loftis, Jr.
Life of this patent
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AssigneeTRW Inc.
InventorsDarwin K. Decker, Charles B. Loftis, Jr.
Estimating the term…
A system for supplying d.c. power to an electrical load, in which such load includes a rechargeable battery, is characterized by a plurality of power sources connected in common to the electrical load, wherein the current generated by the multiple power sources is combined to supply such electrical load. Each of the power sources includes a solar panel and a controlled variable transconductance device, such as a Buck converter, connected in electrical series circuit. A digital processor, including a stored program, coupled to the control inputs of the variable transconductance devices, selectively individually sets the duty cycle of each transconductance device under control of a stored program, whereby the electrical power supplied by said power sources to said electrical load is individually controlled by the digital processor.
A power system for supplying electrical power over a power bus to at least one power consuming electrical device, comprising:
A solar power supply system of the type containing a rechargeable battery clamping a power bus, comprising:
A solar power supply system of the type containing a rechargeable battery clamping a power bus, comprising:
In a power supply system for supplying dc power over a power bus to an electrical load, said system including adc current generating means coupled to said power bus for supplying current to said electrical load with said generating means being interruptable, a rechargeable battery coupled to said power bus for supplying dc current to said bus in the absence of current from said dc current generating means, whereby electrical charge stored in said battery is depleted and receiving charging current from said dc current generating means over said power bus, whereby electrical charge in said battery is replenished, the improvement comprising:
In a power supply system for supplying dc power to an electrical load over a power bus, said power supply system including generating means coupled to said power bus for supplying current to said electrical load with said generating means being of an interruptable characteristic;
A computer controlled solar array type electrical supply system for converting solar energy to electricity and supplying such electricity to an electrical load requiring a predetermined load current, comprising:
A computerized solar array electrical supply system, comprising:
An electrical current sensor for providing an indication of load current magnitude and direction, said current sensor having wide dynamic range comprising:
A computer assisted electrical current sensor for providing an indication of load current magnitude and direction, said current sensor having a wide dynamic range, comprising:
Dependencies are inferred from the claim text.