Performance Analysis of INS/GNSS Integration for Ballistic Missiles Applications

Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System

SIMULATION OF BALLISTIC MISSILE MOTION IN FREE-FLIGHT (BALLISTIC) PHASE USING NAVSTAR (GPS) NAVIGATION MODEL

INS Alignment Using Onboard Computer Software for Missile Trajectory

Performance Enhancement of Low Cost Non-GPS Aided INS for Unmanned Applications

Integrated MEMS-Based IMU/GPS navigation system for motion dynamical vehicles

Fusion of Low-Cost MEMS IMU/GPS Integrated Navigation System

A TERRESTRIAL STRAPDOWN NAVIGATION ALGORITHM

AN APPROACH TOWARDS BALLISTIC MISSILES PERFORMANCE IMPROVEMENT THROUGH THE APPLICATION OF HIGH-SPELT NAVIGATION PROCESSORS

Improvement of CEP Accuracy for Vehicles Re-entry Using INS/GPS/GNSS Integrated System