Computational framework for investigation of aircraft nonlinear dynamics
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.
qualitative theory bifurcation analysis database nonlinear aircraft dynamics continuation method object-oriented model roll-coupling problem