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Proceedings Paper

Active isolation systems
Author(s): Lawrence M. Germann; Avanindra A. Gupta
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Paper Abstract

This paper summarizes microgravity experiments for space platforms and presents test results of a three-axes active isolation demonstration system that has been built and tested. This mount has demonstrated isolation capability down to 0.05 Hz nd a transmissibility curve which provides isolation levels necessary for microgravity and precision pointing aboard space platforms. The system has high-bandwidth inertial servo loops using accelerometers for active disturbance rejection to isolate the payload from external torque disturbances by the utility transfer devices and moving mechanisms.

Paper Details

Date Published: 23 September 1993
PDF: 6 pages
Proc. SPIE 1949, Space Guidance, Control, and Tracking, (23 September 1993); doi: 10.1117/12.157077
Show Author Affiliations
Lawrence M. Germann, Ball Aerospace and Communications Group (United States)
Avanindra A. Gupta, Ball Aerospace and Communications Group (United States)


Published in SPIE Proceedings Vol. 1949:
Space Guidance, Control, and Tracking
George E. Sevaston; Richard H. Stanton, Editor(s)

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