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机译:考虑轨道交变热场的谐波驱动航天器动力学建模与运动精度分析。
State Key Laboratory of Tribology, Department of Mechanical Engineering, Tsinghua University, Beijing, P.R. China;
State Key Laboratory of Tribology, Department of Mechanical Engineering, Tsinghua University, Beijing, P.R. China;
State Key Laboratory of Tribology, Department of Mechanical Engineering, Tsinghua University, Beijing, P.R. China,Department of Mechanical Engineering, Tsinghua University, Beijing 100084, PR. China;
State Key Laboratory of Tribology, Department of Mechanical Engineering, Tsinghua University, Beijing, P.R. China;
School of Material and Mechanical Engineering, Beijing Technology and Business University, Beijing, P.R. China;
Spacecraft manipulator; temperature distribution; harmonic drive; motion precision; thermal analysis;
机译:轨道横向太阳阵列的航天器热替换诱导振动分析
机译:谐波驱动柔性机械手系统的耦合动态建模与参数识别
机译:考虑J_2对低轨道徘徊的J_2扰动的高精度动态模型与控制
机译:建模大型元素温度变形对小型航天器轨道运动动力学的影响
机译:气动拖航演示航天器的姿态相关离轨寿命分析和极轨通信纳米卫星的详细热子系统设计。
机译:使用桌面高谐波光束对单个纳米结构中的热和声动力学进行全场成像
机译:扰动开放轨道中航天器相对运动的建模,动态和控制
机译:由旋转和/或旋转运动引起的航天器轨道加速度驱动的低温液氦晃动动力学