Evaluation of Structural Behaviour of INS Device Installation Design on Unmanned Aerial Vehicle Using Finite Element Method and Modal Testing

Inertial navigation systems are precise devices that used to measure the orientation and accelerations of a platform they integrated. Accuracy measured data is essential due critical role these systems. The way integrated platform, directly affects accuracy. In this paper, case study alternative designs for Navigation device integration on Tactical Unmanned Aerial Vehicle presented. Mechanical behavior given evaluated with Finite Element Analyses Modal Testing, hence appropriate design selected.