Print Email Facebook Twitter Recursive multibody system dynamics: Extensions and verification of REALDYN simulator Title Recursive multibody system dynamics: Extensions and verification of REALDYN simulator Author van Woerkom, P.Th.L.M. Institution National Aerospace Laboratory NLR Date 1992-11-14 Abstract Earlier work on the formulation of an efficient algorithm for the description of the dynamics of a generic, structurally flexible space manipulator, has resulted in a linear recursive, "Order-N" algorithm. It forms the basis for the multi-body simulation program REALDYN at NLR. Various theoretical results obtained since then, have been collected and are described in the present report. They cover the subjects of extension of simulator applicability, of verification of algorithm and of simulator output, and of numerical integration: •the algorithm is extended to account for cases involving prescribed kinematics in some or all of the joints, and prescribed kinematics for some or all of the degrees of freedom of the spacecraft. •the algorithm is rederived using two different principles of mechanics, in order to support verification of the algorithm itself. •system mechanical integrals are derived, in order to support the verification of the simulator program REALDYN. •finally, the finite accuracy of the solution obtained from numerical integration with the Runge-Kutta-4 routine, is interpreted and analyzed in terms of numerically induced damping. This facilitates interpretation of the numerical results obtained. To reference this document use: http://resolver.tudelft.nl/uuid:a9490280-f3c9-4274-b5bd-5e7220f60a5d Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR CR 93007 L Part of collection Aerospace Engineering Reports Document type report Rights (c) 1992 National Aerospace Laboratory NLR Files PDF 93007.pdf 25.13 MB Close viewer /islandora/object/uuid:a9490280-f3c9-4274-b5bd-5e7220f60a5d/datastream/OBJ/view