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SPACE MANIPULATOR CONTROL FOR THE DYMAFLEX FLIGHT EXPERIMENT

机译:DYMAFLEX飞行实验的空间操纵器控制

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Unlike traditional fixed-base manipulators, manipulators used in space are mounted to a spacecraft whichmay 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 willpresent an increasing challenge in the development of suitable control systems. To improve understandingof the dynamics of this coupled system and to demonstrate and validate proposed controllers in the spaceenvironment, the University of Maryland Space Systems Lab is constructing the Dynamic ManipulationFlight Experiment (DYMAFLEX) microsatellite, the development of which is partially funded by theUnited States Air Force University Nanosat Program. Equipped with a high-performance manipulatorrepresenting approximately 14% of the mass of the combined system and having greater rotational inertiaat full extension than the spacecraft itself, the DYMAFLEX vehicle represents the ideal test bed for spacemanipulator dynamics and control. This paper presents an overview of space manipulator control as it relatesto the DYMAFLEX science mission, with simulation results exploring an intended maneuver in Cartesianspace. The mission is designed to provide empirical validation of existing models for the behavior of aspace manipulator as well as to provide a basis for comparison between proposed control strategies to assesstheir strengths and weaknesses in the actual application environment. In this paper, a simple TransposeJacobian controller is compared to more sophisticated approaches, including the Modified Transpose Jacobiancontroller of Papadopoulos and Moosavian. A technique is proposed for mitigating the chattering problemassociated with the MTJ strategy. The effect of measurement noise is explored. An adaptive controller isconsidered as a further means of improving performance. Preliminary conclusions are drawn, to be verifiedon the DYMAFLEX platform.
机译:与传统的固定基座机械手不同,在太空中使用的机械手安装在航天器上, 可能会响应任何力或扭矩而自由移动。这导致高度耦合的动力学系统。 过去,与主机航天器相比,机械臂通常速度较慢且重量较轻。 但是随着经济激励推动小型,更快,更轻型车辆的发展,这种耦合将 在开发合适的控制系统方面提出了越来越大的挑战。增进理解 耦合系统的动力学特性,并演示和验证空间中拟议的控制器 环境,马里兰大学太空系统实验室正在构建动态操纵 飞行实验(DYMAFLEX)微卫星,其开发的部分资金来自 美国空军大学Nanosat计划。配备了高性能机械手 约占组合系统质量的14%,并具有更大的旋转惯量 DYMAFLEX运载工具比航天器本身具有更大的扩展性,是太空的理想测试平台 机械手动力学和控制。本文概述了与之相关的空间机械手控制。 进行DYMAFLEX科学任务,仿真结果探索了笛卡尔的预期操作 空间。该任务旨在对模型的行为进行现有模型的实证验证。 空间操纵器,以及为拟议控制策略之间的比较提供基础,以进行评估 它们在实际应用环境中的优缺点。在本文中,一个简单的移调 将Jacobian控制器与更复杂的方法(包括Modified Transpose Jacobian)进行比较 Papadopoulos和Moosavian的财务总监。提出了一种减轻抖动问题的技术 与MTJ策略相关联。探索了测量噪声的影响。自适应控制器是 被认为是提高绩效的另一种手段。得出初步结论,待核实 在DYMAFLEX平台上。

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