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Quasi-dual-bus satellite power supply controller

A technology of satellite power supply and controller, which is applied in the field of satellite power supply, can solve the problems of heavy weight, large pulse load interference to the bus, and many equipments, so as to reduce production cost, reduce the number of equipment or volume weight, and simplify system configuration. Effect

Inactive Publication Date: 2016-06-01
CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Single busbar design, that is, all loads share one power supply busbar; the advantage is that the number of equipment in the power supply system is small, the volume and weight are small, and the cost is low; The anti-interference ability and the quality requirements of the power system are relatively high
[0004] Double busbar design, that is, two busbars are designed for the power system, one busbar supplies power to stable loads, and the other busbar supplies power to pulsed loads; the advantage is that it can effectively avoid the interference caused by pulsed negatives to stable loads; but there are also many devices in the power supply system , larger weight, higher cost and other disadvantages and problems

Method used

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  • Quasi-dual-bus satellite power supply controller

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Embodiment 1

[0018] See attached figure 1 .

[0019] A quasi-double-bus satellite power controller, which is composed of a charge regulator 5, a discharge regulator 6, a shunt regulator 7, a filter circuit and a control circuit, is characterized in that: the output port of the quasi-double-bus satellite power controller is connected in parallel with a load Filter circuit, the platform bus is output by port I1 and port II2, and the load bus is output by port III3 and port IV4. The load filter circuit connected in parallel to the output port of the quasi-double bus satellite power controller adopts a π-type filter circuit.

[0020] The specific structure and data parameters of this embodiment are described in detail as follows:

[0021] Such as figure 1 As shown in the figure, the configuration of the common power controller is shown in the rectangular box. By configuring a reasonable filter circuit at its output port, the load bus and the platform bus can be isolated to a certain extent,...

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PUM

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Abstract

The invention relates to a quasi-dual-bus satellite power supply controller, and belongs to the technical field of a satellite power supply. The quasi-dual-bus satellite power supply controller comprises a charging regulator (5), a discharging regulator (6), a parallel regulator (7), a filter circuit and a control circuit; the quasi-dual-bus satellite power supply controller is characterized in that the output port of the quasi-dual-bus satellite power supply controller is in parallel connection with a load filter circuit; a platform bus is output by a port I (1) and a port II (2); and a load bus is output by a port III (3) and a port IV (4). The filter circuit is reasonably configured at the output end by the power supply controller provided by the invention, so that the platform bus and the load bus can be isolated to a certain degree; the influence on the platform bus from pulse load generated when the load is in operating is avoided or lowered to the greatest extent; meanwhile, the system configuration can be simplified; and therefore, the quasi-dual-bus satellite power supply controller has the advantages of capabilities of reducing equipment quantity or volume weight, lowering production cost, adapting pulse load special requirements, and the like.

Description

technical field [0001] The invention belongs to the technical field of satellite power supplies, in particular to a quasi-double-bus satellite power supply controller. Background technique [0002] At present, most of the solar-battery power systems of satellites adopt single-bus design. In recent years, due to the requirements of some special loads, the power system is required to have short-term, pulse, and high-power output capabilities; the design of this type of satellite power system adopts a double-bus design, that is, one bus provides power for stable loads, and one Busbars supply pulsed loads. [0003] Single busbar design, that is, all loads share one power supply busbar; the advantage is that the number of equipment in the power supply system is small, the volume and weight are small, and the cost is low; The anti-interference ability and the quality requirements of the power system are relatively high. [0004] Double busbar design, that is, two busbars are de...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H02J7/00
Inventor 赵海峰罗顺王乐乐刘元默马文伟
Owner CHINA ELECTRONIC TECH GRP CORP NO 18 RES INST
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