A new payload integration methodThis 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.
Document ID
19810045032
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Engels, R. C. (Martin Marietta Aerospace Denver, CO, United States)
Harcrow, H. W. (Martin Marietta Aerospace Denver, Colo., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-0501Report Number: AIAA PAPER 81-0501
Meeting Information
Meeting: Conference on Structures, Structural Dynamics and Materials