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A Numerical Method for Computing the State Transition Matrix Using Poincare Integral Invariants The Poincare integral invariants describe the volumes of sets in Hamiltonian phase space. We use these invariants to derive a new numerical procedure for obtaining the state transition matrix (STM), which can be applied to both conservative and nonconservative systems. The method is analogous to a finite difference approximation of the STM, where perturbed states are numerically propagated along with the reference trajectory. We discuss the mathematical similarities between this new STM and existing methods, show numerical results for orbital motion and uncertainty propagation, and discuss new insights afforded by the Hamiltonian properties of phase flow.
Document ID
20240009234
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Michael A Shoemaker
(Goddard Space Flight Center Greenbelt, United States)
Kyle M Hughes
(Goddard Space Flight Center Greenbelt, United States)
Date Acquired
July 19, 2024
Subject Category
Astrodynamics
Report/Patent Number
AAS 24-270
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Broomfield, CO
Country: US
Start Date: August 11, 2024
End Date: August 15, 2024
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: 385616.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
state transition matrix
Hamiltonian
phase space
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