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航天器大功率直流電源數字均流方法
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1.上海航天電子技術(shù)研究所;2.上海交通大學(xué) 計算機科學(xué)與工程系

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V475.1

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Digital Current Sharing Method For High-power DC Power Supply of Spacecraft
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    摘要:

    針對航天器大功率直流電源系統電源模塊的均流問(wèn)題,提出了直流電源系統數字均流方法。該方法以供配電主控軟件為均流核心,將各直流電源模塊進(jìn)行并聯(lián)輸出,通過(guò)以太網(wǎng)與各直流電源模塊進(jìn)行數據交互,采集各直流電源輸出電流,通過(guò)均流算法調節直流電源輸出電壓,以達到電源均流的目的,此方法在現有直流電源的基礎上,設計了大功率直流電源并聯(lián)硬件電路,包含輸入控制單元、遠端補償電路和輸出控制單元,軟件上設計供配電主控軟件,包含均流控制功能、供配電流程功能和電源模塊監控功能。通過(guò)實(shí)際硬件環(huán)境試驗表明,該方法均流精度高、響應速度快、故障控制能力強,在航天電源領(lǐng)域具備較高的實(shí)用價(jià)值。

    Abstract:

    A digital current sharing method for DC power supply systems is proposed to address the current sharing problem of power modules in spacecraft high-power DC power supply systems. This method uses the power supply main control software as the current sharing core, and outputs each DC power module in parallel. It interacts with each DC power module through Ethernet to collect the output current of each DC power supply, and adjusts the output voltage of the DC power supply through the current sharing algorithm to achieve the goal of current sharing. This method is based on the existing DC power supply and designs a high-power DC power supply parallel hardware circuit, which includes input control unit, remote compensation circuit, and output control unit. On the software side, a power supply and distribution main control software is designed, including current sharing control function, power supply and distribution process function, and power module monitoring function.Through actual hardware environment experiments, it has been shown that this method has high current sharing accuracy, fast response speed, and strong fault control ability, and has high practical value in the field of aerospace power supply.

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杜璞玉,陳卓,高飛,王劍,瞿浩.航天器大功率直流電源數字均流方法計算機測量與控制[J].,2024,32(6):319-325.

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歷史
  • 收稿日期:2024-01-17
  • 最后修改日期:2024-02-08
  • 錄用日期:2024-02-20
  • 在線(xiàn)發(fā)布日期: 2024-06-18
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