空间环境测功机(SED)的实验能力与成果

Casey J. Clark, J. D. Smith, Andrew J. Nick, Victoria Ortega, A. Kennett, R. P. Dillon, B. Buckles
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摘要

空间环境测功机(SED)室设计用于开展低温机器人研究;一个研究领域,重点研究在极端寒冷环境下运行的机器人系统和旋转机械,包括地球,近地轨道,火星,月球,小行星,太阳轨道,行星轨道,或在这些目的地之间旅行期间遇到的那些。测试室采用模块化测力计,由各种制动器,扭矩传感器和电机组成,可以在测试之间轻松互换。每个测试都采用独特的测试剖面,在给定的周期或转数中包含不同的施加扭矩和速度设定值。模块化的测功机设置允许任何组合的电机,变速箱进行测试。这个房间是独一无二的,位于美国宇航局肯尼迪航天中心颗粒力学和风化层操作实验室(GMRO)的沼泽工程设施内。其他冷室也存在,但它们是特定于项目的,不能同时输出实时扭矩、温度和效率数据。这种极冷环境测试箱的模块化,加上定制的软件和仪器,使其成为独一无二的。该舱室能够将低温温度和压力稳定到与月球环境相称的水平。针对不同的低温设定值、扭矩和角速度,已经成功地对电机和齿轮箱进行了测试。使用各种温度传感器记录了试验件和试验箱的相关内部温度。通过对各种加热器的PWM信号进行PID增益调度,稳定了被测电机和齿轮箱的温度设定值。电机的散热是通过使用铜带创建一个从低温头直接到测试件的导热路径来提供的。各种应变波齿轮(swg),也称为谐波传动,行星齿轮系统和直流电机执行器配置已在室中进行了测试。所进行的实验是为各种项目进行的,包括大块金属玻璃齿轮(BMGG),挥发性物质研究极地探测车(VIPER),原位资源利用试点挖掘机(IPEX)。为了进行低温机器人研究,对极冷环境试验室进行了各种升级。这些升级通过在硬件和软件中提供冗余,极大地增加了测试设置的自主能力。增加冗余主要是为了保护冷冻头的完整性。采用了一种新的捆扎和绝缘方法来建立从执行器到冷冻头的导热路径。该软件经过升级,包括温度设定值控制,进一步提高了测试的自主能力。本文详细介绍了对极冷环境试验箱的升级,并强调了coldam验收测试的结果。
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Experimental Capabilities and Achievements of the Space Environment Dynamometer (SED)
The Space Environment Dynamometer (SED) chamber was designed to conduct research in cryobotics; an area of study that focuses on robotic systems and rotating machinery operating in extreme cold environments including Earth, low Earth orbit, Mars, Moon, asteroids, Solar orbit, planetary orbit, or those encountered during travel among these destinations. The test chamber incorporates a modular dynamometer, consisting of a variety of brakes, torque sensors and motors to be easily interchanged between tests. Each test employs a unique test profile that incorporates different setpoints of applied torques and velocities for a given period or number of revolutions. The modularity of the dynamometer setup allows for any combination of motor, gearbox to be tested. This chamber is one of a kind and resides at the Swamp Works facility within the Granular Mechanics and Regolith Operations laboratory (GMRO) at NASA Kennedy Space Center. Other cold chambers exist, however they are project specific and do not simultaneously output real time torque, temperature and efficiency data. The modularity of this extreme cold environment test chamber, coupled with the custom software and instrumentation, makes it one of a kind. The chamber is capable of stabilizing cryogenic temperatures and pressures to commensurate moon environments. Tests have successfully been conducted on motors and gearboxes for various cryogenic temperature set points, torques, and angular velocities. Relevant internal temperatures of the test article and chamber were recorded using a variety of temperature sensors. The temperature setpoints, on the motors and gearboxes tested, were stabilized by using PID gain scheduling of the PWM signal for the various heaters. The heat removal for the motor was provided by creating a thermally conductive path from a cryohead directly to the test article using copper straps. A variety of strainwave gears (SWGs), also known as Harmonic drives, planetary gear systems and DC motor actuator configurations have been tested in the chamber. The experiments performed were for various projects including Bulk Metallic Glass Gears (BMGG), Volatiles Investigating Polar Exploration Rover (VIPER), In-Situ Resource Utilization Pilot Excavator (IPEX). Various upgrades have been made to the extreme cold environment test chamber for the use of cryobotic research. These upgrades greatly increased the autonomous capabilities of the test set up by providing redundancies in the hardware and software. The redundancies were primarily added to protect the integrity of the cryohead. A new strapping and insulation method was performed to create the thermal conductive path from the actuators to the cryohead. The software was upgraded to include temperature setpoint control, further increasing the autonomous capabilities of the test. This paper goes into detail regarding the upgrades made to the extreme cold environment test chamber, as well as highlights the results from a COLDArm acceptance test.
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