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Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation DynamicsThis paper discusses a generalized approach to the multi-body separation problems in a launch vehicle staging environment based on constraint force methodology and its implementation into the Program to Optimize Simulated Trajectories II (POST2), a widely used trajectory design and optimization tool. This development facilitates the inclusion of stage separation analysis into POST2 for seamless end-to-end simulations of launch vehicle trajectories, thus simplifying the overall implementation and providing a range of modeling and optimization capabilities that are standard features in POST2. Analysis and results are presented for two test cases that validate the constraint force equation methodology in a stand-alone mode and its implementation in POST2.
Document ID
20080008385
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Toniolo, Matthew D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Tartabini, Paul V.
(NASA Langley Research Center Hampton, VA, United States)
Pamadi, Bandu N.
(NASA Langley Research Center Hampton, VA, United States)
Hotchko, Nathaniel
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 7, 2008
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 46th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 7, 2008
End Date: January 10, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available