A technique is presented for conducting efficient loads analyses of Shuttle-payloads systems with linear or nonlinear attachment interfaces. The technique relies on representing the Space Shuttle and the payloads with physical and modal coordinates. Further, by invoking a standard algorithm of numerical integration of equations of motion, the kinematics of the interface degrees of freedom at a given time are determined without calculating the modes of the combined system involving the Space Shuttle and the payload. If the Shuttle-payloads interface coupling induces a linear dynamic model for the loads analysis, the equations of motion of the Shuttle and the payload are integrated separately step-by-step in time. If the dynamic model is nonlinear, the equations of motion of the Shuttle and the payload are again integrated separately. However, in the latter case an iterative procedure is used within a time step to converge to reliable values of the nonlinear terms of the equations of motion. The usefulness of the proposed technique is demonstrated by conducting a loads analysis for the Shuttle abort landing event with the Inertia Upper Stage (IUS) booster carrying a Tracking and Data Relay Satellite (TDRS) in the payload bay. This combined system has at its interface dry friction and hydraulic nonlinear dampers. For the analysis of this system, the discontinuous signum function used traditionally in modeling dry friction is replaced by an expeditious continuous approximation. Because of its efficiency and versatility, the new technique deserves serious consideration for becoming a standard tool for linear or nonlinear analysis of combined systems, in general, and of Shuttle-payloads systems, in particular.
Skip Nav Destination
Article navigation
July 1990
Research Papers
Efficient Loads Analyses of Shuttle-Payloads Using Dynamic Models With Linear Or Nonlinear Interfaces
P. D. Spanos,
P. D. Spanos
School of Engineering, Rice University, Houston, TX 77251
Search for other works by this author on:
T. T. Cao,
T. T. Cao
Loads and Dynamics Section, NASA, Johnson Space Center, Houston, TX 77058
Search for other works by this author on:
D. A. R. Nelson, Jr.,
D. A. R. Nelson, Jr.
Structural Analysis Department, Lockheed Engineering & Sciences Company, Houston, TX 77058
Search for other works by this author on:
D. A. Hamilton
D. A. Hamilton
Loads and Dynamics Branch, NASA, Johnson Space Center, Houston, TX 77058
Search for other works by this author on:
P. D. Spanos
School of Engineering, Rice University, Houston, TX 77251
T. T. Cao
Loads and Dynamics Section, NASA, Johnson Space Center, Houston, TX 77058
D. A. R. Nelson, Jr.
Structural Analysis Department, Lockheed Engineering & Sciences Company, Houston, TX 77058
D. A. Hamilton
Loads and Dynamics Branch, NASA, Johnson Space Center, Houston, TX 77058
J. Vib. Acoust. Jul 1990, 112(3): 366-373 (8 pages)
Published Online: July 1, 1990
Article history
Received:
June 1, 1989
Revised:
October 1, 1989
Online:
June 17, 2008
Citation
Spanos, P. D., Cao, T. T., Nelson, D. A. R., Jr., and Hamilton, D. A. (July 1, 1990). "Efficient Loads Analyses of Shuttle-Payloads Using Dynamic Models With Linear Or Nonlinear Interfaces." ASME. J. Vib. Acoust. July 1990; 112(3): 366–373. https://doi.org/10.1115/1.2930517
Download citation file:
Get Email Alerts
Cited By
Primary Resonance in a Weakly Forced Oscillator With Both Parametric Damping and Stiffness
J. Vib. Acoust (February 2024)
Reduced-Order Modeling in Rotordynamics and Its Robustness to Random Matrix Perturbation
J. Vib. Acoust (February 2024)
Reviewer's Recognition
J. Vib. Acoust (February 2024)
Related Articles
Dynamic Modeling and Analysis of Spacecraft With Variable Tilt of Flexible Appendages
J. Dyn. Sys., Meas., Control (March,2014)
Use of the Non-Inertial Coordinates in the Analysis of Train Longitudinal Forces
J. Comput. Nonlinear Dynam (January,2012)
Computer Analysis of Machines With Planar Motion: Part 2—Dynamics
J. Appl. Mech (September,1970)
Automatic Model Generation for Modular Reconfigurable Robot Dynamics
J. Dyn. Sys., Meas., Control (September,1998)
Related Proceedings Papers
Related Chapters
Resource-Aware Routing in Interplanetary Mars Surface Network
International Conference on Advanced Computer Theory and Engineering (ICACTE 2009)
On the Exact Analysis of Non-Coherent Fault Trees: The ASTRA Package (PSAM-0285)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)
Discovering Similar Segments by Time-Parameterized Trajectory Clustering
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3