タイトル | Interchangeable end effector tools utilized on the PFMA |
本文(外部サイト) | http://hdl.handle.net/2060/19940022646 |
著者(英) | Littles, Jay; Morrison, Jim; Crow, George; Gierow, Paul; Carroll, John; Maness, Michael; Cody, Joe |
著者所属(英) | Spectra Research Systems, Inc. |
発行日 | 1992-02-27 |
言語 | eng |
内容記述 | An instrumented task board, used for measuring forces applied by the Protoflight Manipulator Arm (PFMA) to the task board, was fabricated and delivered to Marshall Space Flight Center. SRS Technologies phased out the existing IBM compatible data acquisition system, used with a instrumented task board, and integrated the force measuring electronic hardware in with the Macintosh II data acquisition system. The purpose of this change was to acquire all data with the same time tag, allowing easier and more accurate data reduction in addition to real-time graphics. A three-dimensional optical position sensing system for determining the location of the PFMA's end effect or in reference to the center of the instrumented task board was also designed and delivered under. An improved task board was fabricated which included an improved instrumented beam design. The modified design of the task board improved the force/torque measurement system by increasing the sensitivity, reliability, load range and ease of maintenance. A calibration panel for the optical position system was also designed and fabricated. The calibration method developed for the position sensors enhanced the performance of the sensors as well as simplified the installation and calibration procedures required. The modifications made under this effort expanded the capabilities of the task board system. The system developed determines the arm's position relative to the task board and measures the signals to the joints resulting from the operator's control signals in addition to the task board forces. The software and hardware required to calculate and record the position of the PFMA during the performance of tasks with the instrumented task board were defined, designed and delivered to MSFC. PFMA joint input signals can be measured from a breakout box to evaluate the sensitivity or response of the arm operation to control commands. The data processing system provides the capability for post processing of time-history graphics and plots of the PFMA positions, the operator's actions, and the PFMA servo reactions in addition to realtime force and position sensor data presentation. |
NASA分類 | MECHANICAL ENGINEERING |
レポートNO | 94N27149 NASA-CR-193925 NAS 1.26:193925 SRS/STG-TR92-14 REPT-5490-08 |
権利 | No Copyright |
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