作者: J. P. Noel , G. Kerschen , A. Newerla
DOI: 10.1007/978-1-4614-2416-1_1
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摘要: Many nonlinear system identification methods have been introduced in the technical literature during last 30 years. However, few of these were applied to real-life structures. In this context, objective present paper is demonstrate that Restoring Force Surface (RFS) method can provide a reliable spacecraft structure. The component comprises an inertia wheel mounted on support, motion which constrained by eight elastomer plots and mechanical stops. Several adaptations RFS are proposed, include elimination kinematic constraints regularization ill-conditioned inverse problems. proposed methodology demonstrated using numerical data.