摘要
针对FY 1C卫星姿态控制系统 ,给出了系统方案、系统设计、系统特点和飞行试验的结果 ;对一些新的技术设计和新颖特殊的方案特点 ,从理论分析和技术实现给出了设计思路和工程实现的方法 ;分析了FY 1C卫星姿态控制系统在轨运行的结果 ;对长寿命、低成本和稳定连续运行的工程实现进行了研究 ;给出了FY
Based on the attitude control system of FY 1C satellite, the author offers the project, design, characters of the system and the flight results. According to theoretical analysis and technique realization, this article also describes the design and technical realization method for the new technology and the peculiar project characteristics. In addition, the author analyzes the on orbitresults of the FY 1C satellite; makes research on the long life, low cost and continuous stable motion and presents the level and application development of FY 1C satellite's attitude control system.
出处
《上海航天》
2001年第2期33-43,共11页
Aerospace Shanghai
关键词
气象卫星
姿态控制系统
磁控制
三轴稳定
章动进动控制
Mateorological satellite
Attitude control system
Magnetic control
Three axis stabilization
Notation and precession control
