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Multi-axis transient vibration testing of space objects: Test philosophy, test facility, and control strategyIABG has been using various servohydraulic test facilities for many years for the reproduction of service loads and environmental loads on all kinds of test objects. For more than 15 years, a multi-axis vibration test facility has been under service, originally designed for earthquake simulation but being upgraded to the demands of space testing. First tests with the DFS/STM showed good reproduction accuracy and demonstrated the feasibility of transient vibration testing of space objects on a multi-axis hydraulic shaker. An approach to structural qualification is possible by using this test philosophy. It will be outlined and its obvious advantages over the state-of-the-art single-axis test will be demonstrated by example results. The new test technique has some special requirements to the test facility exceeding those of earthquake testing. Most important is the high reproduction accuracy demanded for a sophisticated control system. The state-of-the-art approach of analog closed-loop control circuits for each actuator combined with a static decoupling network and an off-line iterative waveform control is not able to meet all the demands. Therefore, the future over-all control system is implemented as hierarchical full digital closed-loop system on a highly parallel transputer network. The innermost layer is the digital actuator controller, the second one is the MDOF-control of the table movement. The outermost layer would be the off-line iterative waveform control, which is dedicated only to deal with the interaction of test table and test object or non-linear effects. The outline of the system will be presented.
Document ID
19930006409
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lachenmayr, Georg
(Industrieanlagen-Betriebsgesellschaft m.b.H. Ottobrunn, Germany)
Date Acquired
September 6, 2013
Publication Date
November 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, The Seventeenth Space Simulation Conference. Terrestrial Test for Space Success
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N15598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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