<div>The air-breathing hypersonic vehicle (AHV) holds the potential to revolutionize
global travel, enabling rapid transportation to low-Earth orbit and even space
within the next few decades. This study focuses on investigating the nonlinear
dynamic simulation, trim, and stability analysis of a three-degrees-of-freedom
(3DOF) longitudinal model of a generic AHV for variable control surface
deflection, <i>δ<sub>e</sub></i> and <i>δ<sub>r</sub></i>. A
simulation is developed to analyze the burstiness of the AHV’s nonlinear
longitudinal behavior, considering the complete flight envelope across a wide
range of Mach numbers, from <i>M</i> = 0 to 24, for selected stable
<i>M</i>. The presented simulation assesses trim analysis and
explores the dynamic stability of the AHV through its flight envelope and
bifurcation method analysis is carried out to gain insight and validate the
dynamic stability using eigen value approach.</div>