Spark range data reduction using a Gauss collocation method

Author:

Burchett Bradley T1ORCID

Affiliation:

1. CCDC Army Research Laboratory, Aberdeen Proving Ground, MD, USA

Abstract

A new method is proposed for reducing spark range data using a Gauss pseudospectral collocation. Existing methods use numerical integration to propagate the differential equation model and its sensitivities forward in time. Here, a collocation method is used to transcribe the differential equations into algebraic ones that are easily solved. Realizing that the auxiliary equations used to find model sensitivities are linear, a second transcription renders a set of linear algebraic equations that solve exactly for the needed sensitivities without iteration. Thus, measurement sensitivities with respect to initial conditions and aerodynamic parameters are easily found through solution of a set of linear algebraic equations. The method is demonstrated on a set of actual data from the M898 155-mm projectile. For models using fixed-plane coordinates, and only the 10 most influential aerodynamic coefficients, the new method produces results that rival established commercial codes in accuracy.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Reference15 articles.

1. A method for extracting aerodynamic coefficients from free-flight data

2. Hathaway W, Whyte R. Aeroballistic research facility free flight data analysis using the maximum likelihood method. Air Force Armament Laboratory (US)AFATL, 1979, pp. 79–98.

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