Reaction torque minimization techniques for articulated payloadsArticulated payloads on spacecraft, such as antenna telemetry systems and robotic elements, impart reaction torques back into the vehicle which can significantly affect the performance of other payloads. This paper discusses ways to minimize the reaction torques of articulated payloads through command-shaping algorithms and unique control implementations. The effects of reaction torques encountered on Landsat are presented and compared with simulated and measured data of prototype systems employing these improvements.
Document ID
19890043658
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kral, Kevin (Honeywell Sperry Space Systems Glendale, AZ, United States)
Aleman, Roberto M. (NASA Goddard Space Flight Center Greenbelt, MD, United States)