Integrated Navigation System: Strapdown Inertial Navigation and Synthetic Aperture Radar

Integrated navigation program combining strapdown inertial navigation and synthetic aperture radar technologies in geographic coordinate system, with algorithm implementation details

MATLAB Implementation of Strapdown Inertial Navigation System Simulation

Strapdown Inertial Navigation Simulation Program. This simulation targets general aircraft applications, using the geographic coordinate system as the navigation frame. It implements mechanical arrangement and numerical simulation based on north-referenced navigation principles. The guidance system focuses on ballistic missiles, designing standard trajectories and comparing perturbation guidance with explicit guidance methods. The implementation selects flexible and adaptive explicit guidance, utilizing required velocity increment as the cutoff function to control engine shutdown for target impact.

MATLAB Implementation of XYZ to NEU Coordinate Transformation

MATLAB code implementation for converting Earth-Centered Earth-Fixed (ECEF) XYZ coordinates to topocentric North-East-Up (NEU) coordinate system with algorithmic explanations