TY - GEN
T1 - Design of high performance management and control system of nano-satellite for distributed space exploration
AU - Sun, Ke
AU - Fang, Jiancheng
AU - Zhu, Zhuangsheng
AU - Wei, Xuechao
PY - 2008
Y1 - 2008
N2 - Nano-satellite is a kind of advanced and effective tool for space exploration. And the nano-satellite formation flight technology becomes more and more important in distributed space exploration. Thus a design of high performance management and control system (named MCS) of nano-satellite for formation space exploration is presented in this paper. Different with traditional design concept for satellites, MCS adopts a modular configuration not only to satisfy composite requirements of processing capacity, integration, cost and power of nano-satellite, but also to fit applications in formation flight experimentation. MCS includes OBC (on-board computer) module, attitude & orbit control module, telemetry & telecommand module, and power management module. Furthermore, as core component the design uses reconfiguration scheme and COTS (commercial-off-the-shelf) technology, so it shows an outstanding performance in high efficiency, high reliability, low power and low cost for satellite engineering applications.
AB - Nano-satellite is a kind of advanced and effective tool for space exploration. And the nano-satellite formation flight technology becomes more and more important in distributed space exploration. Thus a design of high performance management and control system (named MCS) of nano-satellite for formation space exploration is presented in this paper. Different with traditional design concept for satellites, MCS adopts a modular configuration not only to satisfy composite requirements of processing capacity, integration, cost and power of nano-satellite, but also to fit applications in formation flight experimentation. MCS includes OBC (on-board computer) module, attitude & orbit control module, telemetry & telecommand module, and power management module. Furthermore, as core component the design uses reconfiguration scheme and COTS (commercial-off-the-shelf) technology, so it shows an outstanding performance in high efficiency, high reliability, low power and low cost for satellite engineering applications.
KW - COTS
KW - Formation flight
KW - Management & control system
KW - Reconfiguration
UR - https://www.scopus.com/pages/publications/57649187555
U2 - 10.1117/12.807476
DO - 10.1117/12.807476
M3 - 会议稿件
AN - SCOPUS:57649187555
SN - 9780819473639
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Seventh International Symposium on Instrumentation and Control Technology
T2 - 7th International Symposium on Instrumentation and Control Technology: Optoelectronic Technology and Instruments, Control Theory and Automation, and Space Exploration
Y2 - 10 October 2008 through 13 October 2008
ER -