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套筒驱动的大型可展收柔性太阳翼地面展开重力卸载研究 被引量:9
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作者 杨巧龙 闫泽红 +2 位作者 任守志 宋晓东 何鹏鹏 《载人航天》 CSCD 2017年第4期536-540,545,共6页
大型空间展开机构在微重力环境工作,自身不具备克服地面重力展开的能力,在地面进行展开试验验证时,需对机构进行重力卸载。套筒驱动的大型可展收柔性太阳翼存在在轨展开步骤多路径复杂、活动部件多、收拢构型紧凑而展开尺度大的特点,地... 大型空间展开机构在微重力环境工作,自身不具备克服地面重力展开的能力,在地面进行展开试验验证时,需对机构进行重力卸载。套筒驱动的大型可展收柔性太阳翼存在在轨展开步骤多路径复杂、活动部件多、收拢构型紧凑而展开尺度大的特点,地面重力卸载难以实现。以过程无需调整航天器姿态就完成全部展开步骤为目标,利用气浮法、配重法、悬吊法等对展开过程的不同步骤设计了相应的重力卸载方案。采用特殊构型的工装解决了干涉问题,采用主动牵引的方法消除了工装引入的摩擦力。方案得到地面展开试验验证,具有工程借鉴价值。 展开更多
关键词 柔性太阳翼 重力卸载 气浮法 配重法 悬吊法
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Study on the Behavior of Solar Array Deployment with Root Hinge Drive Assembly 被引量:9
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作者 DING Xilun LI Xin +2 位作者 XU Kun yang qiaolong PU Hailing 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2012年第2期276-284,共9页
In this paper, a method of using a root hinge drive assembly (RHDA) to control the solar array deployment is provided and a multi-DOF mechanism dynamic model of the system is established. In this way, the root hinge... In this paper, a method of using a root hinge drive assembly (RHDA) to control the solar array deployment is provided and a multi-DOF mechanism dynamic model of the system is established. In this way, the root hinge torque can be calculated iteratively. Then taking the predicted torque as a reference, a RHDA is designed for a large multiple-stage packaging and deployable solar array system. The control effect of the drive assembly is validated by ground tests. The test results indicate that the solar arrays can be deployed smoothly, and the deployment velocities are restricted by the drive assembly as expected. During the tests, the RHDA output speed and output torque are obtained. In order to examine the impact force when the yoke is lock-up with a hard stop, dynamics simulations are performed according to the actual behavior. The simulation result indicates that the designed RHDA reduces the impact force significantly and improves the lock-up reliability effectively. 展开更多
关键词 solar array root hinge drive assembly multi-DOF model dynamics simulation reliability lock-up
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