Design of Orbit-Ground Closed Loop PHM System for Spacecraft

DOI

10.2991/wcnme-19.2019.49How to use a DOI?

Keywords

prognostics and health management; spacecraft; architecture

Abstract

The technologies of spacecraft Prognostics and Health Management (PHM) are researched from the architecture and communication protocol. Firstly the spacecraft PHM system is proposed to build with the mode of orbit-ground coordination three-level closed loop. Then, the communication protocol of PHM for spacecraft is designed.

Copyright

© 2019, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Rongzheng Luo
AU  - Zhiyun Tan
AU  - Zhidong Li
AU  - Shuli Yang
AU  - Shuo Feng
AU  - He Gao
PY  - 2019/06
DA  - 2019/06
TI  - Design of Orbit-Ground Closed Loop PHM System for Spacecraft
BT  - Proceedings of the 2019 International Conference on Wireless Communication, Network and Multimedia Engineering (WCNME 2019)
PB  - Atlantis Press
SP  - 205
EP  - 207
SN  - 2352-538X
UR  - https://doi.org/10.2991/wcnme-19.2019.49
DO  - 10.2991/wcnme-19.2019.49
ID  - Luo2019/06
ER  -