NASA NTRS · 19850022874
Parametric Stiffness Control of Flexible Structures
Abstract
An unconventional method for control of flexible space structures using feedback control of certain elements of the stiffness matrix is discussed. The advantage of using this method of configuration control is that it can be accomplished in practical structures by changing the initial stress state in the structure. The initial stress state can be controlled hydraulically or by cables. The method leads, however, to nonlinear control equations. In particular, a long slender truss structure under cable induced initial compression is examined. both analytical and numerical analyses are presented. Nonlinear analysis using center manifold theory and normal form theory is used to determine criteria on the nonlinear control gains for stable or unstable operation. The analysis is made possible by the use of the exact computer algebra system MACSYMA.
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Moon, F. C., Rand, R. H.. 1985-04-01. Parametric Stiffness Control of Flexible Structures. https://ntrs.nasa.gov/citations/19850022874
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