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机译:航天器飞轮微振动隔离系统的建模与分析
College of Aerospace Science and Engineering, National University of Defense Technology, No. 47 Yanwachi Street, Changsha 410073, China;
College of Aerospace Science and Engineering, National University of Defense Technology, No. 47 Yanwachi Street, Changsha 410073, China;
College of Aerospace Science and Engineering, National University of Defense Technology, No. 47 Yanwachi Street, Changsha 410073, China;
College of Aerospace Science and Engineering, National University of Defense Technology, No. 47 Yanwachi Street, Changsha 410073, China;
Microvibration; Flywheel; Passive vibration isolation platform; Gyroscopic effects; Equivalent dynamic model;
机译:航天器多飞轮系统微振动隔离的分析与优化
机译:飞船微轮隔振平台的性能分析
机译:具有陀螺和飞轮多余系统的航天器旋转运动的数学模型及其姿态控制问题。第二部分
机译:宇宙飞船飞轮微振隔离的设计与建模
机译:一种用于航天器微振动源建模和分析的半经验方法。
机译:基于深度生成模型的航天器控制系统异常检测
机译:一种用于航天器微振动源建模和分析的半经验方法。
机译:空气弹簧隔振系统电磁铁定位与微振动控制