The output torque estimation of MCMG for agile satellites
agile、attitude control system、simulation results、attitude maneuver、small satellite、control law、special、torque、design、paper、help
26
O3(力学)
The project was supported by the National Natural Science Foundation of China10872029;Excellent Scholars Fund of Beijing20071D1600300398;北京理工大学优秀青年基金2007YS0202
2010-06-23(万方平台首次上网日期,不代表论文的发表时间)
141-146