摘要
利用MSCAdams中用户自定义子程序方法建立卫星姿态控制系统的模型,对卫星附件在轨展开过程进行卫星姿态动力学仿真分析.
This satellite attitude control system model is established by using MSC Adams user subroutine. The simulation analysis of the satellite attitude dynamics during the process of appurtenances deployment in the space is discussed.
出处
《计算机辅助工程》
2006年第B09期4-5,共2页
Computer Aided Engineering