Mathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process for Safety and Security Issues

TL;DR

This paper develops mathematical models for aerospace Space-to-Surface systems to optimize trajectories and enhance safety by avoiding intercepts, integrating atmospheric, aerodynamic, and guidance models with statistical analysis.

Contribution

It introduces comprehensive mathematical models for Space-to-Surface flight, including atmospheric, aerodynamic, and navigation aspects, with simulation and statistical analysis for intercept avoidance.

Findings

Successful modeling of atmospheric and aerodynamic flight phases

Optimized trajectory planning for intercept avoidance

Statistical validation of model accuracy

Abstract

The research project has been made for mathematical modeling of aerospace system Space-to-Surface for avoid intercepting process by flight objects Surface-to-Air. The research has been completed and created mathematical models which used for research and statistical analysis. In mathematical modeling has been including a few models: Model of atmosphere, Model of speed of sound, Model of flight head in space, Model of flight in atmosphere, Models of navigation and guidance, Model and statistical analysis of approximation of aerodynamic characteristics. Modeling has been created for a Space-to-Surface system defined for an optimal trajectory in terminal phase. The modeling includes models for simulation atmosphere, aerodynamic flight and navigation by an infrared system. The modeling simulation includes statistical analysis of the modeling results.