PENGUKURAN MOMEN INERSIA PADA QUADROTOR PARROT BEBOP 1 DENGAN METODE BIFILAR PENDULUM

• Main Author: Syahid Nugraha, Wildan
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/43059
• Institution: Institut Teknologi Bandung

The knowledge of mathematical models is needed for the purpose of development of UAV control system. In the mathematical modeling of UAV, important parameters with sufficient accuracy are needed, in order to get a precision system model. One of those important parameters is the moment of inertia. There are two approaches that can be used to obtain the moment of inertia model, namely the analytical calculation method and experimental calculation. The experimental test procedure for determining the moment of inertia is divided into two categories, the acceleration and oscillation methods. Various moments of inertia that are included in the oscillation method itself can be divided into two parts based on the recovery force used in the test. There are tests that use springs or other elastic equipment as a restorer, there are also tests that use gravity as the restoration force or commonly called the pendulum method. One of the pendulum methods commonly used to model the moment of inertia of an object is the bifilar pendulum. The results of the bifilar pendulum method compared to analytical calculations show that measuring the moment of inertia by using that method is proven to obtain reliable results with values that can be accounted for.