摘要 : A kinematic scheme is presented which allows for planning attitude manoeuvres of satellites after actuator failure. The scheme relies on the identification of admissible rotation axes around which the control system can deliver to... 展开
作者 | G. Avanzini F. Giulietti |
---|---|
作者单位 | |
期刊名称 | 《Journal of loss prevention in the process industries》 |
总页数 | 8 |
语种/中图分类号 | 英语 / X92 |
关键词 | Satellite attitude control Actuator failure Under-actuated spacecraft |
馆藏号 | N2008EPST0003604 |