Approach determination method using aerodynamic modeling.

Abstract

The invention proposes a method for determining the approach zone using an aerodynamic model. The method utilizes an aerodynamic model that considers lift, air resistance, gravity, and the object's directional control. Under varying initial conditions, the simulation process is repeated to determine spatial points where the object can successfully approach the target and satisfy the given conditions. This set of points constitutes the approach zone, represented as a 2D cross-section or a 3D volume. The method helps to accurately determine the effective impact zone of an object under real-world conditions.

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