航天發(fā)射通用化指顯數(shù)據(jù)處理方法及應(yīng)用
2022年電子技術(shù)應(yīng)用第11期
周 淦,劉貴聰,申展瑜,周 宇
華北計(jì)算機(jī)系統(tǒng)工程研究所,北京100083
摘要: 隨著航天發(fā)射任務(wù)的日趨頻繁、新式飛行器和測控設(shè)備的不斷應(yīng)用以及多級(jí)一體化指揮的迫切需求,對(duì)發(fā)射任務(wù)指揮顯示系統(tǒng)提出了更高的通用性和適應(yīng)性要求。為解決上述問題,提出了一種彈性的指揮顯示數(shù)據(jù)處理方法。該方法通過離線態(tài)定義協(xié)議模型和主題模型,完成數(shù)據(jù)接入內(nèi)外部協(xié)議映射;在線態(tài)采用組件化方式逐級(jí)實(shí)現(xiàn)外部數(shù)據(jù)的接入、解析、存儲(chǔ)與轉(zhuǎn)發(fā)等工作。試驗(yàn)應(yīng)用表明,該方法通過模型的定義實(shí)現(xiàn)了處理邏輯和數(shù)據(jù)協(xié)議的解耦,可在不更動(dòng)平臺(tái)框架的前提下實(shí)現(xiàn)指顯數(shù)據(jù)的靈活快速接入,極大地提高了航天發(fā)射指揮顯示系統(tǒng)的任務(wù)準(zhǔn)備效率。
中圖分類號(hào): TP311;V19
文獻(xiàn)標(biāo)識(shí)碼: A
DOI:10.16157/j.issn.0258-7998.212276
中文引用格式: 周淦,劉貴聰,申展瑜,等. 航天發(fā)射通用化指顯數(shù)據(jù)處理方法及應(yīng)用[J].電子技術(shù)應(yīng)用,2022,48(11):121-126.
英文引用格式: Zhou Gan,Liu Guichong,Shen Zhanyu,et al. General data processing method and application of space launch command and monitoring system[J]. Application of Electronic Technique,2022,48(11):121-126.
文獻(xiàn)標(biāo)識(shí)碼: A
DOI:10.16157/j.issn.0258-7998.212276
中文引用格式: 周淦,劉貴聰,申展瑜,等. 航天發(fā)射通用化指顯數(shù)據(jù)處理方法及應(yīng)用[J].電子技術(shù)應(yīng)用,2022,48(11):121-126.
英文引用格式: Zhou Gan,Liu Guichong,Shen Zhanyu,et al. General data processing method and application of space launch command and monitoring system[J]. Application of Electronic Technique,2022,48(11):121-126.
General data processing method and application of space launch command and monitoring system
Zhou Gan,Liu Guichong,Shen Zhanyu,Zhou Yu
National Computer System Engineering Research Institute of China,Beijing 100083,China
Abstract: With the increasing frequency of space launch missions, constant application of new spacecraft and tracking and control equipment, and the urgent demand of multi-level integrated command, it puts forward higher universality and adaptability requirements for space launch command and monitoring system. In order to solve these problems, this paper proposes a novel flexibility data processing method of command and monitoring system. By defining protocol model and topic model in off-line mode, this method realizes the map of the internal and external communication protocol. On the other hand, the component methodology is adopted to accomplish the receiving, parsing, storing, and transmitting operation of external data in online mode. The experimental results show that this method successfully decouples the processing logic and data protocol by using the definition of various models, achieves the flexible information exchange for command and monitoring data without revising the software architecture, and sharply improves the preparation efficiency of the command and monitoring system for space launch missions.
Key words : space launch;command and monitoring;general;protocol model;topic model
0 引言
近年來,我國航天已進(jìn)入高密度、高強(qiáng)度發(fā)射常態(tài)化階段,發(fā)射任務(wù)的密集化對(duì)發(fā)射場保障能力提出了更加嚴(yán)格的標(biāo)準(zhǔn)和要求。隨著運(yùn)載火箭技術(shù)的不斷發(fā)展和新型高性能測控設(shè)備的列裝應(yīng)用,發(fā)射場如何在飛行器和測控能力調(diào)整的情況下快速適應(yīng)密集任務(wù)成為了一個(gè)值得深究的問題。
與此同時(shí),信息技術(shù)的高速發(fā)展已推動(dòng)我國航天發(fā)射場實(shí)現(xiàn)測發(fā)、測控、氣象、通信和勤務(wù)五大分系統(tǒng)一體化融合,打破了原有各分系統(tǒng)數(shù)據(jù)煙囪式的壁壘,極大提高了發(fā)射場內(nèi)部試驗(yàn)指揮效率。但未來航天發(fā)射場建設(shè)更加趨向于一體化,多個(gè)不同發(fā)射場缺乏統(tǒng)一規(guī)劃的建設(shè)現(xiàn)狀增加了信息的互聯(lián)、互通與互操作的難度。順應(yīng)未來航天發(fā)射任務(wù)一體化試驗(yàn)指揮的建設(shè)趨勢,需迫切解決多個(gè)發(fā)射場信息差異化接入的問題。
本文詳細(xì)內(nèi)容請(qǐng)下載:http://ihrv.cn/resource/share/2000005017。
作者信息:
周 淦,劉貴聰,申展瑜,周 宇
(華北計(jì)算機(jī)系統(tǒng)工程研究所,北京100083)
此內(nèi)容為AET網(wǎng)站原創(chuàng),未經(jīng)授權(quán)禁止轉(zhuǎn)載。