Centralized bus interface with single wire secondary...

Details Centralized bus interface with single wire secondary... Centralized bus interface with single wire secondary...

2003-09-17

2009-02-03

Eldred, J. Woodrow (Department: 3641)

Aeronautics and astronautics

Spacecraft

With payload accommodation

C244S158100

Reexamination Certificate

active

07484693

ABSTRACT:
A system for single wire secondary distribution comprising a spacecraft platform; a central bus interface unit coupled to the spacecraft platform; a payload unit coupled to the central bus interface unit; and a centralized power supply for powering the central bus interface unit and the payload unit; wherein the spacecraft platform provides a command to the central bus interface unit; wherein the central bus interface unit interrupts the power to the payload unit in a manner corresponding to the commands received by the central bus interface unit; wherein the payload unit decodes the interruption to the power and executes the command from the spacecraft platform.

REFERENCES:
patent: 7027483 (2006-04-01), Santhoff et al.

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