Abstract:
This project is basically about designing and manufacturing the fuselage and landing gear system for an UAV. The fuselage must be able to withstand the vibration create from the engine. While the landing gear must be able to support the weight of the engine and all other component. Due to the vibration, a dampener will be installed at certain location to reduce the vibration on the UAV.
I will be focusing on the fuselage construction and landing gear configuration, Weight is the most important aspect that need to be taken in consideration. With a proper materials and designing we could reduce some weight and aid in the aerodynamic of the aircraft. After everything were completed, a vibration testing will be carried out to test the vibration before and after installation of the dampener.
