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Ins gps integration - PowerPoint PPT Presentation

Inertial navigation

Inertial navigation. Basic principle. If we can measure the acceleration of a aircraft we can integrate the acceleration to get velocity integrate the velocity to get position deviation. X B = X A +dX Y B = Y A +dY Z B = Z A +dZ. Z. A(X A ,Y A ,Z A ). dX. dY. dZ. B(X B ,Y B ,Z B ).

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Ins gps integration - PowerPoint PPT Presentation

Inertial navigation