Ballistic Navigation Solution Using GPS/INS Integration

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

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

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

INS Alignment Using Onboard Computer Software for Missile Trajectory

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

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

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

Performance Analysis of Strapdown Inertial Navigation Algorithms

ERROR ANALYSIS OF INERTIAL NAVIGATION SYSTEMS