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Simulation of a spatial, servo-hydraulic test facility for space structuresIn this paper different control concepts for servo-hydraulic test facilities are derived using exact linearization techniques. Based on different linear and nonlinear models of the test table and the actuator dynamics several nonlinear controllers of different complexity are derived. The closed loop system performance of the controlled servo-hydraulic test facility is tested in various computer simulations using both, standard test signals and large test signals as system inputs. The simulation results turn out, that in case of standard input signals the test facility controller must include a linear test table mechanics model and a nonlinear servo-hydraulic actuator model. Additional simulations demonstrate the robustness of the control concept selected for standard test signals with respect to variations of plant parameters.
Document ID
19950007682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leimbach, K.-D.
(Kassel Univ.)
Hahn, H.
(Kassel Univ.)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Publication Information
Publication: NASA. Goddard Space Flight Center, Eighteenth Space Simulation Conference: Space Mission Success Through Testing
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
95N14095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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