I. Introduction
Unmanned aerial vehicles, or drones, are categorized by fixed wings or rotary wings. The flight of drones with rotary wings depends on the operation of the rotors that are spatially distributed along multiple intersected axes and represented by the structure of the circular k-out-of-n: G balanced system. If some rotors fail during flight, the other rotors must work harder to maintain velocity, and we infer that the drone's weight will affect operational efficiency. Thus, a load-sharing dependency occurs because the operating rotors share the load equally.