How to mitigate the integration error in numerical simulations of Newtonian systems

Pini Gurfil, Itzik Klein

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

We introduce a method for eliminating the truncation error produced when numerically integrating an initial value problem using Runge-Kutta-based algorithms. We propose a methodology for constructing an optimal state-space representation that gives zero local numerical truncation error, and in this sense, is the optimal state-space representation for modeling given phase-space dynamics. To that end, we utilize a simple transformation of the state-space equations into their variational form. This process introduces an inherent freedom, similar to the gauge freedom in physics. We then utilize the gauge function to eliminate the numerical truncation error. We show that by choosing an appropriate gauge function the numerical integration error dramatically decreases and one can achieve much better accuracy compared to the standard state variables for a given time-step. Moreover, we derive general expressions yielding the optimal gauge functions given a Newtonian one degree-of-freedom ODE. For the n degrees-of-freedom case we describe a MATLAB® code capable of finding the optimal gauge functions and integrating the given system using the gauge-optimized integration algorithm. In all of our illustrating examples, the gauge-optimized integration outperforms the integration using standard state variables by a few orders of magnitude.

Original languageEnglish
Title of host publicationTechnion Israel Institute of Technology - 46th Israel Annual Conference on Aerospace Sciences 2006
Pages95-130
Number of pages36
StatePublished - 2006
Externally publishedYes
Event46th Israel Annual Conference on Aerospace Sciences 2006 - Tel-Aviv, Haifa, Israel
Duration: 1 Mar 20062 Mar 2006

Publication series

NameTechnion Israel Institute of Technology - 46th Israel Annual Conference on Aerospace Sciences 2006
Volume1

Conference

Conference46th Israel Annual Conference on Aerospace Sciences 2006
Country/TerritoryIsrael
CityTel-Aviv, Haifa
Period1/03/062/03/06

Keywords

  • Gauge theory
  • Initial value problems
  • Linear ordinary differential equations
  • Variation of parameters

ASJC Scopus subject areas

  • General Computer Science
  • Space and Planetary Science
  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • General Physics and Astronomy

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