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NASA NTRS · 19810045032

A new payload integration method

Abstract

This paper introduces a new payload integration method. The system equations of motion are derived in terms of interface-restrained booster and payload modes. These system equations are directly integrated, avoiding the solution of an expensive eigenvalue problem. A modified Newmark-Chan-Beta numerical scheme is used to perform this integration. Due to the unique form of the system equations it is possible to achieve significant savings. A similar savings is feasible for the computation of the internal loads. This new approach does not involve approximations. Although completely general, the presented technique is most effective when the number of interface degrees of freedom is relatively small. Both determinate and indeterminate interfaces are allowed.

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BibTeXRIS

Engels, R. C., Harcrow, H. W.. 1981-01-01. A new payload integration method. https://ntrs.nasa.gov/citations/19810045032

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