Numerical bifurcation analysis using continuation methods has emerged as a valuable component in the analysis of mathematical models described by differential equations.The application of bifurcation analysis to flight control problems began in the early 1980s[1].So far.numerical continuation has been employed many times for the analysis of particular flight regimes, although its industrial applications remain quite limited.In several publications bifurcation analysis has been posed as a method for clearance (i.e.verification) of modern flight control laws as well as a supplementary tool for their design[1,2,3].