首页> 外文OA文献 >Next-Generation Maneuvering System with Control-Moment Gyroscopes for Extravehicular Activities Near Low-Gravity Objects
【2h】

Next-Generation Maneuvering System with Control-Moment Gyroscopes for Extravehicular Activities Near Low-Gravity Objects

机译:具有控制力矩陀螺的下一代操纵系统,用于低重力物体附近的舱外活动

摘要

Looking ahead to the human exploration of Mars, NASA is planning for exploration of near-Earth asteroids and the Martian moons. Performing tasks near the surface of such low-gravity objects will likely require the use of an updated version of the Manned Maneuvering Unit (MMU) since the surface gravity is not high enough to allow astronauts to walk, or have sufficient resistance to counter reaction forces and torques during movements. The extravehicular activity (EVA) Jetpack device currently under development is based on the Simplified Aid for EVA Rescue (SAFER) unit and has maneuvering capabilities to assist EVA astronauts with their tasks. This maneuvering unit has gas thrusters for attitude control and translation. When EVA astronauts are performing tasks that require ne motor control such as sample collection and equipment placement, the current control system will re thrusters to compensate for the resulting changes in center-of-mass location and moments of inertia, adversely affecting task performance. The proposed design of a next-generation maneuvering and stability system incorporates control concepts optimized to support astronaut tasks and adds control-moment gyroscopes (CMGs) to the current Jetpack system. This design aims to reduce fuel consumption, as well as improve task performance for astronauts by providing a sti er work platform. The high-level control architecture for an EVA maneuvering system using both thrusters and CMGs considers an initial assessment of tasks to be performed by an astronaut and an evaluation of the corresponding human-system dynamics. For a scenario in which the astronaut orbits an asteroid, simulation results from the current EVA maneuvering system are compared to those from a simulation of the same system augmented with CMGs, demonstrating that the forces and torques on an astronaut can be significantly reduced with the new control system actuation while conserving onboard fuel.
机译:展望人类对火星的探索,美国宇航局正在计划探索近地小行星和火星卫星。在这样低重力物体的表面附近执行任务可能需要使用更新版本的有人操纵单元(MMU),因为其表面重力不足以使宇航员能够行走,或者没有足够的抵抗反作用力的能力运动中的扭矩。当前正在开发的机外活动(EVA)Jetpack设备基于EVA救援简化援助(SAFER)单元,并具有机动能力以协助EVA宇航员完成任务。该操纵单元具有气体推进器,用于姿态控制和平移。当EVA宇航员执行需要电机控制的任务(例如样品收集和设备放置)时,当前的控制系统将重新推进器,以补偿质量中心位置和惯性矩的变化,从而对任务性能产生不利影响。拟议的下一代机动和稳定系统设计融合了为支持宇航员任务而优化的控制概念,并为当前的Jetpack系统增加了控制力矩陀螺仪(CMG)。该设计旨在通过提供更佳的工作平台来减少燃油消耗,并改善宇航员的任务性能。同时使用推进器和CMG的EVA操纵系统的高级控制体系结构考虑了对宇航员要执行的任务的初始评估以及对相应人机系统动力学的评估。对于宇航员绕小行星运行的情况,将当前EVA操纵系统的仿真结果与同一系统的仿真结果进行了比较,该仿真系统使用CMG进行了增强,表明新的航天器可以显着降低宇航员上的力和扭矩控制系统的驱动,同时节省车载燃油。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

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