Electromagnetic compatibility of MARS Orbiter Mission spacecraft

Vaddi Raghavaiah,P Sowjanya,R L Mini,P V N Murthy, S M Muniraja,R Renuka, G K Rama Murali, D Binu, Santhi Sankaranarayanan,V Senthil Kumar,B S Srinivas, V K Hariharan, V V Srinivasan

Microwave and RF Conference(2014)

引用 4|浏览1
暂无评分
摘要
The MARS Orbiter Mission (MOM) spacecraft carries on-board sensitive receiver and high gain antenna system to cater to the requirement of inter-planetary and deep space communication. This paper describes, among others, the stringent EMC requirements for MOM spacecraft, summary of EMC analysis carried out, modification on subsystem level EMI/EMC test limit and EMI/ESD mitigation techniques followed to achieve EMC compliance of MOM Spacecraft.
更多
查看译文
关键词
artificial satellites,electromagnetic compatibility,interference suppression,radio receivers,satellite antennas,space communication links,emc analysis,emc requirements,emc test limit,emi mitigation technique,esd mitigation technique,mars orbiter mission spacecraft,mom spacecraft,deep space communication,high gain antenna system,interplanetary communication,on-board sensitive receiver,emi/emc/esd,electromagnetic interference,method of moments,mars
AI 理解论文
溯源树
样例
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要