Development Of Six-Degree Of Freedom Strapdown Terrestrial INS Algorithm

Many of accurate inertia) guided missile systems iced to use more complex mathematical calculations and require a high speed processing to ensure the real-time operation. This will give rise to the need of developing an efficient high-speed computing system with modern inertial guided algorithms, In this work, a flexible computer simulation program for the terrestrial slrapi own INS algorithm was developed and implemented lor six-degree of freedom m ssile flight simulator. The evaluation of the algorithm is 1 vised on (he accuracy of the proposed algorithm with real data.