Mathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process

TL;DR

This paper presents a mathematical model for aerodynamic space-to-surface flight, focusing on optimal trajectory planning to avoid interception, incorporating atmospheric, aerodynamic, and infrared navigation models with statistical analysis.

Contribution

It introduces a comprehensive modeling framework for space-to-surface flight that optimizes trajectory to evade interception, integrating atmospheric, aerodynamic, and infrared navigation models.

Findings

Successful simulation of the flight model

Statistical analysis validates the model accuracy

Trajectory optimization enhances interception avoidance

Abstract

Modeling has been created for a Space-to-Surface system defined for an optimal trajectory for targeting in terminal phase with avoids an intercepting process. The modeling includes models for simulation atmosphere, speed of sound, aerodynamic flight and navigation by an infrared system. The modeling and simulation includes statistical analysis of the modeling results.