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电磁干扰（EMI）抑制技术是保证航天器各功能单元正常运行互不干扰的重要技术。开关电源是航天器内电磁干扰的主要来源。基于对星载开关电源DC/DC和负载点电源POL电磁干扰特性的测试结果，提出了一种星载二次电源系统的电磁干扰抑制方案，采用高稳晶振+控制器+时钟管理芯片硬件与软件设计结合的方法，利用高稳晶振为电源模块提供稳定时钟，通过控制器实现时钟管理芯片的分频和时钟分配。系统以非同步方式上电，软件控制时钟管理芯片输出电源模块同步时钟，然后软件打开时钟同步的使能，实现星载开关电源（DC/DC和POL）开关频率的外同步，最后通过测量输出电压频谱的方法验证了电磁干扰抑制方案的有效性。

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Copyright of Chemical Engineering of Oil & Gas / Shi You Yu Tian Ran Qi Hua Gong is the property of PetroChina Southwest Oil & Gas Field Company and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)