Research on multicopter nowadays is rapidly growing in many fields of application. One of
the problems in the multicopter application is the ability to lift a heavy load that requires the
careful design and selection of the proper type of multicopter for its ability in carrying out the
missions involving the heavy load lifting. One type of multicopters that is often used is
hexacopter. This paper describes the design of hexacopter that lift a heavy load. The design
is done by calculating and analyzing the constraints and the criteria by the aid of software …

This work presents a methodology of design for multirotor unmanned aerial vehicle (UAV).
The problem on the drone are to overcome the stability of the structure and the blade design
for the drone. The objective for this thesis are to design and analysis the heavy-lifting
Hexacopter drone structure and to measure thrust produce by the designed blade. The
method of design and analysis are done by using software SOLIDWORKS in this project to
simulate the stress and displacement of the structure of the Hexacopter drone. The load …