NASA NTRS · 19900046983
Inverse dynamics of adaptive structures used as space cranes
Abstract
As a precursor to the real-time control of fast moving adaptive structures used as space cranes, a formulation is given for the flexibility induced motion relative to the nominal motion (i.e., the motion that assumes no flexibility) and for obtaining the open loop time varying driving forces. An algorithm is proposed for the computation of the relative motion and driving forces. The governing equations are given in matrix form with explicit functional dependencies. A simulator is developed to implement the algorithm on a digital computer. In the formulations, the distributed mass of the crane is lumped by two schemes, vz., 'trapezoidal' lumping and 'Simpson's rule' lumping. The effects of the mass lumping schemes are shown by simulator runs.
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Das, S. K., Utku, S., Wada, B. K.. 1990-01-01. Inverse dynamics of adaptive structures used as space cranes. https://ntrs.nasa.gov/citations/19900046983
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