Modeling of aerodynamic Space-to-Surface flight with optimal trajectory for targeting

TL;DR

This paper presents a comprehensive model for aerodynamic Space-to-Surface flight, focusing on optimal trajectory planning for targeting, incorporating atmospheric, aerodynamic, and infrared navigation models, with statistical analysis of simulation results.

Contribution

It introduces an integrated modeling framework for Space-to-Surface flight with optimal trajectory planning, including atmospheric and infrared navigation models, and provides statistical analysis of simulation outcomes.

Findings

Successful simulation of aerodynamic flight with optimal targeting trajectory

Validation of atmospheric and infrared navigation models

Statistical analysis demonstrating model robustness

Abstract

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