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SPACE MANIPULATOR CONTROL FOR THE DYMAFLEX FLIGHT EXPERIMENT

机译:Dymaflex飞行实验的空间机械手控制

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Unlike traditional fixed-base manipulators, manipulators used in space are mounted to a spacecraft which may move freely in response to any forces or torques. This results in a highly coupled dynamical system. In the past, robotic arms have often been slow and lightweight in comparison to their host spacecraft; but as economic incentives drive the development of smaller, faster, lighter vehicles, this coupling will present an increasing challenge in the development of suitable control systems. To improve understanding of the dynamics of this coupled system and to demonstrate and validate proposed controllers in the space environment, the University of Maryland Space Systems Lab is constructing the Dynamic Manipulation Flight Experiment (DYMAFLEX) microsatellite, the development of which is partially funded by the United States Air Force University Nanosat Program. Equipped with a high-performance manipulator representing approximately 14% of the mass of the combined system and having greater rotational inertia at full extension than the spacecraft itself, the DYMAFLEX vehicle represents the ideal test bed for space manipulator dynamics and control. This paper presents an overview of space manipulator control as it relates to the DYMAFLEX science mission, with simulation results exploring an intended maneuver in Cartesian space. The mission is designed to provide empirical validation of existing models for the behavior of a space manipulator as well as to provide a basis for comparison between proposed control strategies to assess their strengths and weaknesses in the actual application environment. In this paper, a simple Transpose Jacobian controller is compared to more sophisticated approaches, including the Modified Transpose Jacobian controller of Papadopoulos and Moosavian. A technique is proposed for mitigating the chattering problem associated with the MTJ strategy. The effect of measurement noise is explored. An adaptive controller is considered as a further means of improving performance. Preliminary conclusions are drawn, to be verified on the DYMAFLEX platform.
机译:与传统的固定基础操纵器不同,空间中使用的操纵器安装在航天器上,这些航天器可以响应任何力或扭矩而自由移动。这导致高耦合的动力系统。在过去,与他们的宿主航天器相比,机器人手臂往往缓慢而轻巧;但随着经济激励措施推动开发较小,更快,较轻的车辆,这种耦合将在合适的控制系统的发展中提出越来越大的挑战。为了提高对该耦合系统的动态和在空间环境中展示和验证建议控制器的理解,马里兰州太空系统实验室正在构建动态操纵飞行实验(DymaFLEX)微卫星,其开发部分由此资助美国空军大学纳斯坦特计划。高性能机械手,高性能机械手代表组合系统质量的大约14%,并且在全延伸时具有比航天器本身更大的旋转惯性,Dymaflex车辆代表空间机械手动力学和控制的理想测试床。本文概述了空间操纵器控制,因为它与DymaFLEX科学使命有关,模拟结果探索了笛卡尔空间中的预期换气。该特派团旨在为现有模型提供对空间机械手的行为的实证验证,以及为评估实际应用环境中的优势和缺点的提出控制策略之间的比较提供基础。在本文中,将简单的转置雅培控制器与更复杂的方法进行比较,包括Papadopoulos和Moosavian的改良转置雅培控制器。提出了一种用于减轻与MTJ策略相关的抖动问题的技术。探索了测量噪声的效果。自适应控制器被认为是提高性能的进一步手段。初步结论被绘制,在DymaFLEX平台上进行验证。

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