Reaction Torque Minimization Techniques for Articulated Payloads
International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada === Articulated 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 o...
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International Foundation for Telemetering
1988
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ndltd-arizona.edu-oai-arizona.openrepository.com-10150-6150822016-07-01T03:01:06Z Reaction Torque Minimization Techniques for Articulated Payloads Kral, Kevin Aleman, Robert M. Honeywell-Sperry Space Systems Goddard Space Flight Center International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada Articulated 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. These disturbances can degrade the quality of the data obtained by other on board experiments and systems. 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 the LANDSAT satellite are presented and compared with simulated and measured data of prototype systems employing these improvements. 1988-10 text Proceedings 0884-5123 0074-9079 http://hdl.handle.net/10150/615082 http://arizona.openrepository.com/arizona/handle/10150/615082 International Telemetering Conference Proceedings en_US http://www.telemetry.org/ Copyright © International Foundation for Telemetering International Foundation for Telemetering |
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International Telemetering Conference Proceedings / October 17-20, 1988 / Riviera Hotel, Las Vegas, Nevada === Articulated 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. These disturbances can degrade the quality of the data obtained by other on board experiments and systems. 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 the LANDSAT satellite are presented and compared with simulated and measured data of prototype systems employing these improvements. |
author2 |
Honeywell-Sperry Space Systems |
author_facet |
Honeywell-Sperry Space Systems Kral, Kevin Aleman, Robert M. |
author |
Kral, Kevin Aleman, Robert M. |
spellingShingle |
Kral, Kevin Aleman, Robert M. Reaction Torque Minimization Techniques for Articulated Payloads |
author_sort |
Kral, Kevin |
title |
Reaction Torque Minimization Techniques for Articulated Payloads |
title_short |
Reaction Torque Minimization Techniques for Articulated Payloads |
title_full |
Reaction Torque Minimization Techniques for Articulated Payloads |
title_fullStr |
Reaction Torque Minimization Techniques for Articulated Payloads |
title_full_unstemmed |
Reaction Torque Minimization Techniques for Articulated Payloads |
title_sort |
reaction torque minimization techniques for articulated payloads |
publisher |
International Foundation for Telemetering |
publishDate |
1988 |
url |
http://hdl.handle.net/10150/615082 http://arizona.openrepository.com/arizona/handle/10150/615082 |
work_keys_str_mv |
AT kralkevin reactiontorqueminimizationtechniquesforarticulatedpayloads AT alemanrobertm reactiontorqueminimizationtechniquesforarticulatedpayloads |
_version_ |
1718328670601347072 |