English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Tools annual

Global: Zendy Free Plan

Global: Zendy Tools monthly

Global: Zendy Plus monthly

The communications link in a space program is a crucial point for upgrading its performance by handling data\udbetween spacecraft bus and payloads, because spacecraft’s missions are related to the data handling mechanism\udusing communications ports such as a controlled area network bus (CAN Bus) and a universal asynchronous receiver\udand transmitter (UART). The NEXTSat-1 has a lot of communications ports for performing science and technology\udmissions. However, the top level system requirements for the NEXTSat-1 are mass and volume limitations. Normally,\udthe communications for units shall be conducted by using point to point link which require more mass and volume to\udinterconnect. Thus, our approach for the novel communications link in the NEXTSat-1 program is to use CAN and serializer\udand deserializer low voltage differential signal (SerDesLVDS) to meet the system requirements of mass and volume.\udThe CAN Bus and SerDesLVDS were confirmed by using already defined communications link for our missions in the\udNEXTSat-1 program and the analysis results were reported in this study in view of data flow and size analysis

Communications Link Design and Analysis of the NEXTSat-1 for SoH File and Mission Data Using CAN Bus, UART and SerDesLVDS