• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>IEEE Aerospace Conference >Concepts of active payload modules and end-effectors suitable for standard interface for Robotic Manipulation of Payloads in Future Space Missions (SIROM) interface
【24h】

Concepts of active payload modules and end-effectors suitable for standard interface for Robotic Manipulation of Payloads in Future Space Missions (SIROM) interface

机译：适用于标准接口的有源有效载荷模块和末端执行器的概念，这些标准接口用于未来太空任务（SIROM）接口中的机器人操纵有效载荷

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

The increasing variety of space missions, combined with their rising complexity and need for more environmentally-friendly, yet cost-effective, solutions, is putting the traditional spacecraft and rover designs to the test. In fact, the majority of nowadays spacecraft and planetary rovers are mostly monolithic, one-of-a-kind, single-use systems, hardly offering any possibility for their future servicing, upgrade or re-use. The EU-funded H2020 project Standard Interface for Robotic Manipulation of Payloads in Future Space Missions (SIROM) aims to bridge this gap by developing an integrated and inherently optimized multi-functional standard interface for mechanical, data, electrical and thermal transfer. The interface, in combination with a custom end-effector and active payload modules (APMs), will allow designing modular and re-configurable systems that could be easily serviced and upgraded via a dedicated robotic system for in-orbit or planetary environment. With respect to the existing state-of-the-art, the interface and modules in SIROM are being developed considering the need for scalability, reusability, compatibility with robotic manipulation and suitability for both environments. Within this context, the paper aims to analyze the feasibility of APM and end-effector concepts, within the system requirements of the project, in order to identify their most suitable preliminary concepts. The analysis is performed in terms of functionalities and architecture, and in case of APMs, considers a remote sensing and power storage system as payloads for orbital and planetary scenarios, respectively. The methodology used for the evaluation of APM and end-effector concepts is a top-down methodology generally used for the design and sizing of payloads of space missions. It consists of: (a) definition of payload objectives and its desired capabilities, (b) identification of candidates, (c) estimation of their characteristics based on analogy, scaling or component budgeting, and (d) evaluation and selection of a reference concept. Moreover, in case of the end-effector analysis, interactions and configurations with APM concepts were also taken into consideration. The results of the analysis point out the feasibility of APMs and end-effectors, within the system requirements of the project, and outline concepts that could be used in the future steps of the project as a guideline in the detailed design of APMs and end-effectors.
机译：越来越多的太空任务，再加上复杂性的提高，以及对更环保，更具成本效益的解决方案的需求，正在对传统的航天器和漫游者设计进行测试。实际上，当今的大多数航天器和行星漫游车大多是整体的，唯一的，一次性使用的系统，几乎无法为它们的未来维修，升级或再利用提供任何可能性。欧盟资助的H2020项目“未来太空飞行中的机器人有效载荷操纵标准接口”（SIROM）旨在通过开发一种集成且固有优化的多功能机械，数据，电和热传递标准接口来弥合这一差距。该界面与定制的末端执行器和有源有效载荷模块（APM）结合使用，将允许设计模块化和可重新配置的系统，这些系统可以通过专用的机器人系统轻松地进行维修和升级，以用于在轨或行星环境。关于现有的最新技术，考虑到对可伸缩性，可重用性，与机器人操纵的兼容性以及对两种环境的适用性的需求，正在开发SIROM中的接口和模块。在此背景下，本文旨在在项目的系统需求内分析APM和终端执行器概念的可行性，以便确定它们最合适的初步概念。该分析是从功能和体系结构方面进行的，对于APM，分别将遥感和电力存储系统视为轨道和行星情况的有效载荷。用于评估APM和末端执行器概念的方法是自上而下的方法，通常用于太空任务有效载荷的设计和规模确定。它包括：（a）有效载荷目标及其所需能力的定义，（b）候选者的识别，（c）根据类比，缩放或组件预算估算其特性，以及（d）评估和选择参考概念。此外，在末端执行器分析的情况下，还考虑了与APM概念的交互和配置。分析结果指出了APM和最终执行者在项目系统要求内的可行性，并概述了可在项目的未来步骤中使用的概念，作为APM和最终设计的详细设计的指南效应器。

著录项

相似文献

  • 外文文献
  • 专利
获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

  • 客服微信

  • 服务号