Abstract
To extract physical output from dynamic reduced models output transformation matrices (OTM) are needed. The OTMs are based on the modal displacement method in combination with the mode acceleration approach. The derivation of load transformation matrix (LTM), the displacement transformation matrix (DTM), etc. is presented in this chapter.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
19.3 References
Bray, E.L., May 1991, Specification for Dynamic Models of Polar Platform, British Aerospace Ltd., Earth Observation and Science Division, SPE-1211368-003, Issue 3.
Chung, Y.T., 1998, Dynamic Loads Recovery using Alternative Mode Acceleration Approach, AIAA-98-1719, 39th AIAA/ASME/ASCE/AHS/ASC/Structures, Structural Dynamics, and Materials Conference and Exhibit and AIAA/ASME/AHS Adaptive Structures Forum, Long Beach, California, April 20–23, 1998.
Craig, R.R, Jr. Bampton, M.C.C., July 1968, Coupling of Substructures for Dynamic Analysis, AIAA Journal, Vol. 6 No. 7, pages 1313–1319.
Craig, R.R, Jr., 1981, Structural Dynamics, An Introduction to Computer Methods, John Wiley & Sons, ISBN 0-471-04499-7.
Fransen, S.H.J.A., 2002, An Overview and Comparison of OTM Formulations on the Basis of the Mode Displacement Method and the Mode Acceleration Method, paper 17, Proceedings of the Worldwide Areospace Conference and Technology Showcase 2002, 810 April, 2002, Toulouse.
Klein, M., Reynolds, J., Ricks, E., 1988, Derivation of improved load transformation matrices for launchers-spacecraft coupled analysis, and direct computation of margins of safety, Proc. Int. Conf.: “Spacecraft Structures and Mechanical testing”, Noordwijk, The Netherlands, 1921 October 1988, pages 703–719.
Rights and permissions
Copyright information
© 2008 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
(2008). Output Transformation Matrices. In: Spacecraft Structures. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-75553-1_19
Download citation
DOI: https://doi.org/10.1007/978-3-540-75553-1_19
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-75552-4
Online ISBN: 978-3-540-75553-1
eBook Packages: EngineeringEngineering (R0)