首页> 外文会议>54th Israel annual conference on aerospace sciences : program >STABILITY ANALYSIS AND TESTING OF A DOCKING SIMULATOR
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STABILITY ANALYSIS AND TESTING OF A DOCKING SIMULATOR

机译:停泊模拟器的稳定性分析和测试

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摘要

The European Proximity Operation Simulator (EPOS) aims, amongrnother objectives, at performing tests for verification and validation of therndocking phase of an on-orbit servicing mission. The simulator includesrntwo robots, equipped with very accurate position controllers, holdingrna docking interface, a probe element, and (virtual) satellites. A keyrnfeature of the simulator set-up is a feedback loop that is closed on thernreal force and torque sensed at the docking interface during the contactrnwith the probe and that is used to drive a free-floating bodies numericalrnsimulation. The high stiffness of the controlled robots causes the con-rntact dynamics to be quicker than the robots’ dynamics. This leads torninconsistencies in the docking simulation results and to potential insta-rnbility and damage of the closed-loop system. This work presents a novelrnmitigation strategy to the given challenge, accompanied with a stabilityrnanalysis and validating experiments. The high stiffness issue is addressedrnby combining a virtual stiffness and damping in the software with a realrnstiffness in the hardware, designing, thus, a “hybrid” docking simulator.rnNonlinear state-space modeling of the closed-loop system is performedrnfor the three dimensional case, where the tracking robots system is ap-rnproximated as a pure delay. A linearized model is developed for the tworndimensional case and a simplified expression is obtained by defining asrnstates the depth and the rate of penetration along the normal to therncontact surface. A stability analysis is then performed, easily extendingrnprevious results obtained in single-dimension, which provides stabilityrnregions as a function of the contact stiffness and damping, the trackingrnrobots time delay, and the satellites masses. The design of a hardwarerncompliance device is presented and the effective stiffness along the nor-rnmal to the contact surface is developed. The proposed hybrid contactrndynamics model and the accompanying analysis are envisioned to enablernsafe and flexible docking simulation. The proposed simulator shall en-rnable the emulation of a desired contact dynamics for any stiffness andrndamping characteristics within the stability region.
机译:除其他目标外,欧洲接近运行模拟器(EPOS)的目的是执行测试,以验证和确认在轨维修任务的对接阶段。该模拟器包括两个机器人,这些机器人配备了非常精确的位置控制器,holdna扩展坞接口,探针元件和(虚拟)卫星。模拟器设置的一个关键功能是一个反馈回路,该回路在与探头接触期间在对接界面上感测到的实际力和转矩作用下闭合,并用于驱动自由浮动体的数值模拟。受控机器人的高刚度使其接触动力学比机器人动力学快。这会导致对接仿真结果不一致,并导致潜在的不稳定性和闭环系统的损坏。这项工作提出了针对给定挑战的新型缓解策略,并进行了稳定性分析和验证实验。通过将软件中的虚拟刚度和阻尼与硬件中的真实刚度相结合,解决了高刚度问题,从而设计了“混合”对接模拟器。对于三维情况,对闭环系统进行了非线性状态空间建模,其中跟踪机器人系统被近似为纯延迟。针对二维情况开发了线性化模型,并通过定义沿垂直于接触面的法线的深度和穿透率来获得简化表达式。然后进行稳定性分析,轻松扩展一维获得的先前结果,该结果提供了根据接触刚度和阻尼,跟踪机器人的时间延迟以及卫星质量而定的稳定性区域。提出了硬件兼容装置的设计,并开发了沿标准尺寸到接触表面的有效刚度。设想了所提出的混合接触动力学模型和伴随的分析,以实现安全和灵活的对接仿真。对于在稳定区内的任何刚度和阻尼特性,建议的仿真器应允许仿真所需的接触动力学。

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  • 来源
  • 会议地点 Haifa(IL);Tel Aviv(IL)
  • 作者单位

    DLR - German Aerospace Center, 82234 Wessling, Germany melak.zebenay@dlr.de;

    DLR - German Aerospace Center, 82234 Wessling, Germany toralf.boge@dlr.de;

    Ben-Gurion University of the Negev, POB 653, 84105, Beer-Sheva, Israel danielch@exchange.bgu.ac.il;

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