This paper presents an analysis of the trajectory for the AGM-65B Maverick missile. The missile's performance is governed by the equations of motion, which are fundamental to understanding its dynamics. This work offers a detailed analysis of the flight dynamics for the AGM-65B missile. It concludes that, while solving the governing equations is relatively straightforward, obtaining accurate aerodynamic data and the missile's mass and inertia properties poses a greater challenge. The study focuses on the path of an air-to-surface missile attacking a fixed target. The missile is required to strike the target from above, adhering to the missile's dynamic and trajectory constraints. The problem is approached using optimal control theory, leading to the formulation of a minimum integrated altitude trajectory. This formulation incorporates nonlinear, three-dimensional missile flight dynamics, along with specific boundary conditions and path constraints. The resulting optimal trajectory provides insight into how the range, altitude, and lateral deflection (Y-axis) vary over time. The trajectory is computed numerically using a computer code that calculates the missile's position at any given time.................... Keyword:................Path , Missile , Wing , mass , Velocity, Thrust , Drag , Lift , Angle of attack , Altitude , Force, Distance .