To reduce the cost and improve the reliability of micro-satellites,a method which employing magnetic torques as the only actuators was developed to realize three axis stable control.Then by using linear quadratic regulator(LQR)optimal control theory,the infinite time state regulator and steady gain regulator were designed to stabilize micro-satellite to nadir pointing using fully magnetic torques.Meanwhile,taking KaiTuo-1 satellite in-orbit flight as the research object,the product of inertia,orbit inclinat...
【更新日期】
2017-09-22
【分类号】
V448.2
【正文快照】
引用格式:袁勤,寇义民,季艳波,等.微小卫星三轴稳定磁控算法工程应用[J].中国空间科学技术,2017,37(4):28-33.YUAN Q,KOU Y M,JI Y B,et al.Engineering application of micro-satellite 3-axis stable control with only magnetic actuators[J].Chinese Space Science and Tec
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