Journal of Aerospace Science and Technology

Journal of Aerospace Science and Technology

NORMAL FORM SOLUTION OF REDUCED ORDER OSCILLATING SYSTEMS

Author
Isfahan Univ.
Abstract
This paper describes a preliminary investigation into the use of normal form theory for modelling large non-linear dynamical systems. Limit cycle oscillations are determined for simple two-degree-of-freedom double pendulum systems. The double pendulum system is reduced into its centre manifold before computing normal forms. Normal forms are obtained using a period averaging method which is applicable to non-autonomous systems, more advantageous than the classical methods. Good agreement is observed between the predicted results from the normal form theory and numerical simulations of the original system.

Volume 3, Issue 3
September 2006
Pages 153-158

  • Receive Date 20 June 2009
  • Accept Date 30 October 2017
  • First Publish Date 30 October 2017