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多衛(wèi)星測(cè)控系統(tǒng)的設(shè)計(jì)與實(shí)現(xiàn)
網(wǎng)絡(luò)安全與數(shù)據(jù)治理
楊歡,姬勝凱,王碩,張姍,李斌
華北計(jì)算機(jī)系統(tǒng)工程研究所
摘要: 隨著我國衛(wèi)星制造和發(fā)射技術(shù)的不斷成熟,衛(wèi)星數(shù)量快速增加,傳統(tǒng)的單星測(cè)控系統(tǒng)已逐漸無法滿足當(dāng)前的國內(nèi)需求。為解決測(cè)控系統(tǒng)資源緊張的問題,提出了多衛(wèi)星測(cè)控系統(tǒng)設(shè)計(jì)方案,在滿足傳統(tǒng)測(cè)控系統(tǒng)任務(wù)的基礎(chǔ)上,進(jìn)一步提高了測(cè)控資源利用率。設(shè)計(jì)方案以CPU為主控制器,實(shí)現(xiàn)多衛(wèi)星測(cè)控?cái)?shù)據(jù)的協(xié)議處理,同時(shí)通過管理、控制調(diào)度FPGA完成測(cè)控?cái)?shù)據(jù)的安全傳輸,搭建多衛(wèi)星測(cè)控系統(tǒng)硬件平臺(tái)并進(jìn)行系統(tǒng)測(cè)試。通過對(duì)多衛(wèi)星測(cè)控系統(tǒng)硬件平臺(tái)的測(cè)試,驗(yàn)證了多衛(wèi)星測(cè)控系統(tǒng)的安全性和可靠性。
中圖分類號(hào):TN918.4文獻(xiàn)標(biāo)識(shí)碼:ADOI:10.19358/j.issn.2097-1788.2024.09.014
引用格式:楊歡,姬勝凱,王碩,等.多衛(wèi)星測(cè)控系統(tǒng)的設(shè)計(jì)與實(shí)現(xiàn)[J].網(wǎng)絡(luò)安全與數(shù)據(jù)治理,2024,43(9):84-88.
Design and implementation of multi-satellite measurement and control system
Yang Huan,Ji Shengkai,Wang Shuo,Zhang Shan,Li Bin
National Computer System Engineering Research Institute of China
Abstract: With the continuous maturity of satellite manufacturing and launching technology and the rapid increase in the number of satellites in China, the traditional single satellite measurement and control system has gradually been unable to meet the current domestic demand. To solve the problem of resource shortage of measurement and control system, this paper presents a design scheme of multi-satellite measurement and control system。On the basic of satisfying the tasks of traditional measurement and control system, the scheme also improves the utilization rate of measurement and control resources.The scheme uses CPU as the main controller,and realizes the protocol processing of multi-satellite measurement and control data, at the same time, the secure transmission of measurement and control data is completed through measurement, control and scheduling FPGA. According to the design scheme, the hardware platform of multi-satellite measurement and control system is built, and the system test is carried out. By testing the hardware platform of multi-satellite measurement and control system, the security and reliability of the multi-satellite measurement and control system is verified.
Key words : satellite; measurement and control system; security; communication protocol

引言

近幾年來,隨著我國 “一箭多星”衛(wèi)星互聯(lián)網(wǎng)關(guān)鍵技術(shù)的突破,衛(wèi)星發(fā)射成本大大降低,極大地提升了我國衛(wèi)星發(fā)射的經(jīng)濟(jì)效益[1]。隨著我國電子元器件和航天科技等技術(shù)的快速發(fā)展,衛(wèi)星的研制成本與生產(chǎn)周期不斷降低,使得我國的衛(wèi)星發(fā)射數(shù)量飛速增加,其中很多涉及了多衛(wèi)星測(cè)控領(lǐng)域,進(jìn)一步推動(dòng)了多衛(wèi)星測(cè)控行業(yè)的發(fā)展。作為衛(wèi)星互聯(lián)網(wǎng)產(chǎn)業(yè)的重要組成部分,多衛(wèi)星測(cè)控領(lǐng)域規(guī)模在不斷擴(kuò)大,測(cè)控任務(wù)也日趨復(fù)雜,這對(duì)地面衛(wèi)星測(cè)控系統(tǒng)處理能力提出了更高的要求[2]。與此同時(shí),衛(wèi)星測(cè)控?cái)?shù)據(jù)在傳輸過程中還面臨被截獲、破譯、刪除或篡改等安全風(fēng)險(xiǎn)。在衛(wèi)星互聯(lián)網(wǎng)飛速發(fā)展的今天,提高資源利用率并兼顧安全性已逐漸成為當(dāng)前地面測(cè)控系統(tǒng)的重要發(fā)展方向。

本文提出的多衛(wèi)星測(cè)控系統(tǒng)基于“CPU+FPGA”架構(gòu)方案,為解決地面測(cè)控系統(tǒng)所遇到的多星測(cè)控?cái)?shù)據(jù)并行處理及安全性問題提供了一個(gè)基本思路[3]。該方案以CPU為主控中樞,完成測(cè)控?cái)?shù)據(jù)的協(xié)議處理以及對(duì)FPGA的管理配置,可實(shí)現(xiàn)多顆衛(wèi)星的動(dòng)態(tài)加載和卸載,以滿足并行處理需求。同時(shí)利用FPGA高速的邏輯運(yùn)算能力同時(shí)完成多顆衛(wèi)星測(cè)控?cái)?shù)據(jù)的加解密處理,最終實(shí)現(xiàn)多衛(wèi)星測(cè)控系統(tǒng)。


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作者信息:

楊歡,姬勝凱,王碩,張姍,李斌

(華北計(jì)算機(jī)系統(tǒng)工程研究所,北京100083)


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