Computational framework for investigation of aircraft nonlinear dynamics

  • Authors:
  • M. G. Goman;A. V. Khramtsovsky

  • Affiliations:
  • De Montfort University, Leicester, England LE1 9BH, United Kingdom;De Montfort University, Leicester, England LE1 9BH, United Kingdom

  • Venue:
  • Advances in Engineering Software
  • Year:
  • 2008

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Abstract

A computational framework based on qualitative theory, parameter continuation and bifurcation analysis is outlined and illustrated by a number of examples for inertia-coupled roll maneuvers. The focus is on the accumulation of computed results in a special database and its incorporation into the investigation process. Ways to automate the investigation of aircraft nonlinear dynamics are considered.