摘要
主要针对机载卫星通信系统中 ,极化轴受机体姿态角扰动的数学模型进行了分析与仿真 ,为极化轴的稳定控制、系统实现“动中通”
Mainly analyzes and simulates the mathematical model of which the polaxis is disturbed by attitude angle of the fuselage in airborne satellite communication system and provides the theoretical basis for stability control of polaxis and communication in motion of system .
出处
《现代电子技术》
2002年第11期47-49,共3页
Modern Electronics Technique
