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机译:补偿时变磁矩,以精确控制纳米和微型卫星飞行任务中的姿态
Intelligent Space Systems Laboratory, 608, Department of Aeronautics and Astronautics, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan;
Nakajima-Sako Laboratory, Department of Electrical and Electronic Engineering, Division of Science and Technology, Graduate School, Shinshu University, 4-17-1, Wakasato, Nagano 380-8553, Japan;
Intelligent Space Systems Laboratory, 608, Department of Aeronautics and Astronautics, The University of Tokyo, 7-3-1, Hongo, Bunkyo-ku, Tokyo 113-8656, Japan;
magnetic disturbance decreasing; nano-satellite; attitude control;
机译:磁偶极矩估计和补偿可在纳米卫星任务中进行精确的姿态控制
机译:地球人工卫星磁飞轮姿态控制系统摄动力矩的自动补偿
机译:利用低地球轨道中的空间等离子体的电磁转矩干扰器干扰的用于纳米和微卫星的磁等离子体去轨系统
机译:磁偶极矩估计和补偿,可在纳米卫星任务中进行精确的姿态控制
机译:精确测量正子介子异常磁矩。
机译:单云台控制力矩陀螺仪用圆光栅的标定补偿和精度分析
机译:利用微分几何解耦方法精确控制磁悬浮双万向节矩陀螺仪