Satellite-borne digital load power distribution architecture
A power distribution structure and digital technology, applied in the direction of electrical components, circuit devices, and adjustment of electrical variables, to achieve high power distribution efficiency, facilitate miniaturization, and meet power demand effects
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[0027] In order to make the objectives, technical solutions and advantages of the present invention clearer, a spaceborne digital load power distribution architecture provided by the present application will be described in further detail below with reference to the accompanying drawings.
[0028] The primary bus voltage of a typical satellite is usually 24V / 48V / 100V. Some satellites use unregulated or semi-regulated control methods, and the primary bus has a certain fluctuation range, such as 28-37V, 34-42V, etc. The digital load stand-alone usually requires lower voltages such as 1V, 3.3V or 5V. From the typical voltage of the primary bus of the satellite power supply to the several-volt level voltage requirements of the digital load, it needs to go through voltage regulation links such as voltage regulation, isolation, and voltage transformation.
[0029] The voltage regulation and variable ratio power distribution architecture adopted in the present invention divides the v...
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