The invention discloses an operation method for a Wiener satellite three-dimensional attitude pointing telescopic mechanism. The invention relates to an operation method of a telescopic mechanism, and aims to solve the problems that in the prior art, micro-nano satellite attitude control is high in cost and large in power consumption, and the increasing requirements of on-orbit load multi-task, low power consumption, low cost, light weight, capability of ensuring system safety and reliability by utilizing minimum resource allocation and the like cannot be met. The invention discloses an operation method for a Wiener satellite three-dimensional attitude pointing telescopic mechanism. The method is realized according to the following steps: step 1, connecting the telescopic mechanism; 2, a telescopic rod driving piece and a gravity gradient telescopic rod are assembled; thirdly, a driving motor assembly is installed; fourthly, a transmission mechanism is installed; 5, the telescopic mechanism is driven to stretch out; and 6, the telescopic mechanism is driven to contract. The method is applied to the field of spacecraft control.
一种用于维纳卫星三维姿态指向伸缩机构的操作方法。本发明涉及一种伸缩机构的操作方法,本发明为解决现有技术中微纳卫星姿态控制的成本高、功耗大、不能满足日益提高的在轨载荷多任务、低功耗、低成本、轻量化、能够利用最少的资源配置保证系统安全可靠等需求的问题,一种用于维纳卫星三维姿态指向伸缩机构的操作方法,所述方法是按照以下步骤实现的:步骤一:连接伸缩机构;步骤二:组装伸缩杆驱动件和重力梯度伸缩杆;步骤三:安装驱动电机组件;步骤四:安装传动机构;步骤五:驱动伸缩机构伸出;步骤六:驱动伸缩机构收缩。本发明用于航天器控制领域。
Operation method for Wiener satellite three-dimensional attitude pointing telescopic mechanism
一种用于维纳卫星三维姿态指向伸缩机构的操作方法
2024-03-26
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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