Missile Simulation Data and Proportional Navigation Analysis

Based on missile simulation data, this study visualizes ideal trajectory curves that clearly display ballistic characteristics. Differential equations for proportional navigation are derived, and a 3D trajectory simulation model is established. Simulations are conducted for proportional navigation, incremental proportional navigation, quadratic optimal guidance law, and dynamic-characteristic-considered quadratic optimal guidance law. The research calculates missile-target encounter times, performs comparative analysis, and demonstrates the superiority of the dynamic-characteristic-considered quadratic optimal guidance law through trajectory visualization and performance metrics.

Proportional Navigation Ideal Trajectory Simulation

MATLAB code for proportional navigation ideal trajectory simulation, providing differential equations of proportional navigation method. The implementation uses MATLAB programming language to conduct 3D data simulation of missile ideal trajectories, generates 3D ideal trajectory plots, and analyzes trajectory characteristics under varying missile and target parameters with computational approach explanations.